diff --git a/GameData/RealismOverhaul/RO_SuggestedMods/HabTech2/RO_HabTech2_Cargo.cfg b/GameData/RealismOverhaul/RO_SuggestedMods/HabTech2/RO_HabTech2_Cargo.cfg
new file mode 100644
index 0000000000..e1db2737ae
--- /dev/null
+++ b/GameData/RealismOverhaul/RO_SuggestedMods/HabTech2/RO_HabTech2_Cargo.cfg
@@ -0,0 +1,314 @@
+//	================================================================================
+//	HabTech2 Cargo
+//	================================================================================
+
+
+//	Note:
+//	All of these parts are Item Parts, no known masses, being left at their
+//	default masses. I have no idea what to do with these parts, configuring it
+//	but letting the Kerbalism or Scansat experts figure out what to do with it.
+
+
+//	================================================================================
+//	Racks
+//	================================================================================
+
+
+//	Centrifuge
+@PART[ht2_ISPR_S_centrifuge]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	%ROCargoConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS-RACK Centrifuge Experiment Station
+	@manufacturer = NASA Ames
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Centrifuge
+@PART[ht2_ISPR_S_combustionChamber]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	%ROCargoConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS-RACK Combustion Chamber Experiment Station
+	@manufacturer = NASA Marshall Spaceflight Center
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Freezer
+@PART[ht2_ISPR_S_freezer]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	%ROCargoConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS-RACK Sub-Zero Experiment Facility
+	@manufacturer = #roMfrESA
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Kerbnet Access Station
+@PART[ht2_ISPR_U_kerbNet]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	%ROCargoConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS-RACK KerbNet Access Station
+	@manufacturer = #roMfrESA
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	MechJeb
+@PART[ht2_ISPR_U_mechJeb]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	%ROCargoConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS-RACK MechJeb Terminal
+	@manufacturer = #roMfrIBM
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Remote Command Station
+@PART[ht2_ISPR_U_probeControl]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	%ROCargoConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS-RACK Telerobotics Operator Station
+	@manufacturer = #roMfrIBM
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Command Station
+@PART[ht2_ISPR_U_probeCore]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	%ROCargoConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS-RACK Command Station
+	@manufacturer = #roMfrIBM
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Radio Antenna
+@PART[ht2_ISPR_U_radio]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	%ROCargoConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS-RACK Radio Antenna
+	@manufacturer = #roMfrIBM
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Robotics
+@PART[ht2_ISPR_U_robotics]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	%ROCargoConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS-RACK Robotics Work Station
+	@manufacturer = Canadian Space Agency (CSA)
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Avionics Rack
+@PART[ht2_ISPR_U_SAS]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	%ROCargoConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS-RACK Avionics Rack
+	@manufacturer = #roMfrIBM
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Training Station
+@PART[ht2_ISPR_U_XP]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	%ROCargoConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS-RACK Astronaut Training Station
+	@manufacturer = NASA
+	@description = Standard utility rack part. Allows Astronauts with sufficient XP to be levelled up when installed.
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	================================================================================
+//	Sample Containers
+//	================================================================================
+
+
+//	Bio Level 1
+@PART[ht2_sample_bioLvl1]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	%ROCargoConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS-SCI Arachnid Experiment Terrarium
+	@manufacturer = NASA
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Bio Level 2
+@PART[ht2_sample_bioLvl2]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	%ROCargoConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS-SCI Experiment Aquarium
+	@manufacturer = NASA
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Bio Level 3
+@PART[ht2_sample_bioLvl3]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	%ROCargoConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS-SCI Rodent Experiment Terrarium
+	@manufacturer = NASA
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Chem Level 1
+@PART[ht2_sample_chemLvl1]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	%ROCargoConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS-SCI Experimental Alloy Sample
+	@manufacturer = NASA
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Chem Level 2
+@PART[ht2_sample_chemLvl2]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	%ROCargoConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS-SCI Crystal Growth Package
+	@manufacturer = NASA
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Chem Level 3
+@PART[ht2_sample_chemLvl3]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	%ROCargoConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS-SCI Superconductor Sample
+	@manufacturer = NASA
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Mystery Goo
+@PART[ht2_sample_goo]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	%ROCargoConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS-SCI Mystery Goo Sample Container
+	@manufacturer = NASA
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Physics Level 1
+@PART[ht2_sample_physLvl1]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	%ROCargoConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS-SCI Fluid Sample Sample Container
+	@manufacturer = NASA
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Physics Level 2
+@PART[ht2_sample_physLvl2]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	%ROCargoConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS-SCI Radioactive Material Sample Container
+	@manufacturer = NASA
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Physics Level 3
+@PART[ht2_sample_physLvl3]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	%ROCargoConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS-SCI Nanoparticle Sample Container
+	@manufacturer = NASA
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
\ No newline at end of file
diff --git a/GameData/RealismOverhaul/RO_SuggestedMods/HabTech2/RO_HabTech2_Hanger.cfg b/GameData/RealismOverhaul/RO_SuggestedMods/HabTech2/RO_HabTech2_Hanger.cfg
new file mode 100644
index 0000000000..806a0cee98
--- /dev/null
+++ b/GameData/RealismOverhaul/RO_SuggestedMods/HabTech2/RO_HabTech2_Hanger.cfg
@@ -0,0 +1,37 @@
+//	=========================================================================================================
+//	HabTech 2 Garage
+//	=========================================================================================================
+
+
+//	Garage
+@PART[Garage]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Orbital Construction Garage
+	@manufacturer = NASA
+	@description = External Hangar for Orbital Assembly. Designed to be assembled on orbit for use. No instruction Manual provided
+	@mass = 20
+	@specLevel = concept
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+}
+
+
+//	Mini Garage
+@PART[GarageMini]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Orbital Construction Garage (Short)
+	@manufacturer = NASA
+	@description = Smaller Scale External Hangar for Orbital Assembly. Designed to be assembled on orbit for use. No instruction Manual provided
+	@mass = 10
+	@specLevel = concept
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+}
\ No newline at end of file
diff --git a/GameData/RealismOverhaul/RO_SuggestedMods/HabTech2/RO_HabTech2_IVA.cfg b/GameData/RealismOverhaul/RO_SuggestedMods/HabTech2/RO_HabTech2_IVA.cfg
new file mode 100644
index 0000000000..417e6e972f
--- /dev/null
+++ b/GameData/RealismOverhaul/RO_SuggestedMods/HabTech2/RO_HabTech2_IVA.cfg
@@ -0,0 +1,146 @@
+// ================================================================================
+// HabTech2 IVAs
+// ================================================================================
+
+
+//	BEAM
+@INTERNAL[ht2_beamIVA]:FOR[RealismOverhaul]
+{
+	%scaleAll = 1.8, 1.8, 1.8
+	@MODULE[InternalSeat],*
+	{
+		%kerbalScale = 1.0, 1.0, 1.0
+		%kerbalOffset = 0.0, 0.0, 0.0
+		%kerbalEyeOffset = 0.0, 0.0, 0.0
+	}
+}
+
+
+//	Cupola
+@INTERNAL[ht2_cupolaIVA]:FOR[RealismOverhaul]
+{
+	%scaleAll = 1.8, 1.8, 1.8
+	@MODULE[InternalSeat],*
+	{
+		%kerbalScale = 1.0, 1.0, 1.0
+		%kerbalOffset = 0.0, 0.0, 0.0
+		%kerbalEyeOffset = 0.0, 0.0, 0.0
+	}
+}
+
+
+//	Destiny
+@INTERNAL[ht2_destinyIVA]:FOR[RealismOverhaul]
+{
+	%scaleAll = 1.8, 1.8, 1.8
+	@MODULE[InternalSeat],*
+	{
+		%kerbalScale = 1.0, 1.0, 1.0
+		%kerbalOffset = 0.0, 0.0, 0.0
+		%kerbalEyeOffset = 0.0, 0.0, 0.0
+	}
+}
+
+
+//	Generic Medium
+@INTERNAL[ht2_genericMediumIVA]:FOR[RealismOverhaul]
+{
+	%scaleAll = 1.8, 1.8, 1.8
+	@MODULE[InternalSeat],*
+	{
+		%kerbalScale = 1.0, 1.0, 1.0
+		%kerbalOffset = 0.0, 0.0, 0.0
+		%kerbalEyeOffset = 0.0, 0.0, 0.0
+	}
+}
+
+
+//	Generic Short
+@INTERNAL[ht2_genericShortIVA]:FOR[RealismOverhaul]
+{
+	%scaleAll = 1.8, 1.8, 1.8
+	@MODULE[InternalSeat],*
+	{
+		%kerbalScale = 1.0, 1.0, 1.0
+		%kerbalOffset = 0.0, 0.0, 0.0
+		%kerbalEyeOffset = 0.0, 0.0, 0.0
+	}
+}
+
+
+//	Harmony
+@INTERNAL[ht2_harmonyIVA]:FOR[RealismOverhaul]
+{
+	%scaleAll = 1.8, 1.8, 1.8
+	@MODULE[InternalSeat],*
+	{
+		%kerbalScale = 1.0, 1.0, 1.0
+		%kerbalOffset = 0.0, 0.0, 0.0
+		%kerbalEyeOffset = 0.0, 0.0, 0.0
+	}
+}
+
+
+//	Kibo
+@INTERNAL[ht2_kiboIVA]:FOR[RealismOverhaul]
+{
+	%scaleAll = 1.8, 1.8, 1.8
+	@MODULE[InternalSeat],*
+	{
+		%kerbalScale = 1.0, 1.0, 1.0
+		%kerbalOffset = 0.0, 0.0, 0.0
+		%kerbalEyeOffset = 0.0, 0.0, 0.0
+	}
+}
+
+
+//	Docking Orb
+@INTERNAL[ht2_orbIVA]:FOR[RealismOverhaul]
+{
+	%scaleAll = 1.8, 1.8, 1.8
+	@MODULE[InternalSeat],*
+	{
+		%kerbalScale = 1.0, 1.0, 1.0
+		%kerbalOffset = 0.0, 0.0, 0.0
+		%kerbalEyeOffset = 0.0, 0.0, 0.0
+	}
+}
+
+
+//	Quest
+@INTERNAL[ht2_questIVA]:FOR[RealismOverhaul]
+{
+	%scaleAll = 1.8, 1.8, 1.8
+	@MODULE[InternalSeat],*
+	{
+		%kerbalScale = 1.0, 1.0, 1.0
+		%kerbalOffset = 0.0, 0.0, 0.0
+		%kerbalEyeOffset = 0.0, 0.0, 0.0
+	}
+}
+
+
+//	Lab Node
+@INTERNAL[ht2_sciNodeIVA]:FOR[RealismOverhaul]
+{
+	%scaleAll = 1.8, 1.8, 1.8
+	@MODULE[InternalSeat],*
+	{
+		%kerbalScale = 1.0, 1.0, 1.0
+		%kerbalOffset = 0.0, 0.0, 0.0
+		%kerbalEyeOffset = 0.0, 0.0, 0.0
+	}
+}
+
+
+//	Unity
+@INTERNAL[ht2_unityIVA]:FOR[RealismOverhaul]
+{
+	%scaleAll = 1.8, 1.8, 1.8
+	@MODULE[InternalSeat],*
+	{
+		%kerbalScale = 1.0, 1.0, 1.0
+		%kerbalOffset = 0.0, 0.0, 0.0
+		%kerbalEyeOffset = 0.0, 0.0, 0.0
+	}
+}
\ No newline at end of file
diff --git a/GameData/RealismOverhaul/RO_SuggestedMods/HabTech2/RO_HabTech2_greebles.cfg b/GameData/RealismOverhaul/RO_SuggestedMods/HabTech2/RO_HabTech2_greebles.cfg
new file mode 100644
index 0000000000..b31094a710
--- /dev/null
+++ b/GameData/RealismOverhaul/RO_SuggestedMods/HabTech2/RO_HabTech2_greebles.cfg
@@ -0,0 +1,350 @@
+//	================================================================================
+//	HabTech2 Greebles
+//	================================================================================
+
+
+//	Camera Mast
+@PART[ht2_cameraMast]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS External Camera & Lighting Assembly
+	@manufacturer = NASA
+	@description = This mast features a CCTV camera & powerful lighting system on a pan/tilt head with 360 degrees of rotation. Ideal for providing illumination and monitoring during spacewalks.
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Cargo Bay
+@PART[ht2_cargoBag]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Cargo Storage Bag
+	@manufacturer = NASA Goddard
+	@description = Storage Bag for EVA Equipment.
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	CTC Bay
+@PART[ht2_CTC]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Cargo Transfer Container
+	@manufacturer = NASA Goddard
+	@description = Storage Bag for EVA Equipment.
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Logistics Carrier
+@PART[ht2_ELC]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Express Logistics Carrier
+	@manufacturer = NASA Goddard
+	@description = The ELC are four un-pressurized attached payloads, some designed by the Brazilian Space Agency,[2] for the International Space Station (ISS) that provides mechanical mounting surfaces, electrical power, and command and data handling services for science experiments on the ISS.
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	External Stowage Platform
+@PART[ht2_ESP]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS External Stowage Platform
+	@manufacturer = NASA Goddard
+	@description = External stowage platforms (ESPs) are key components of the International Space Station (ISS). Each platform is an external pallet that can hold spare parts, also known as orbital replacement units (ORUs), for the space station.
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	FPMU
+@PART[ht2_FPMU]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Floating Potential Measurement Unit (FPMU)
+	@manufacturer = NASA Goddard
+	@description = The Floating Potential Measurement Unit is used to measure the electrical and plasma environment around a spacecraft. Especially useful for large structures that spend a long time in space and may build up a significant electrical charge.
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	JEM Communications
+@PART[ht2_JEM_ICS]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS JEM ICS (Inter-orbit Communication System)
+	@manufacturer = #roMfrJAXA
+	@description = Inter-Orbit Communication System (ICS) provides an independent intercommunications network between Kibo and the Tsukuba Space Center
+	@mass = 0.2172
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	!MODULE[ModuleDataTransmitter],* {}
+	MODULE
+	{
+		name = ModuleRealAntenna
+		referenceGain = 2
+		RFBand = UHF //	Default
+	}
+}
+
+
+//	JEM MCE
+@PART[ht2_JEM_MCE]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS JEM MCE (Multi-mission Consolidated Equipment)
+	@manufacturer = #roMfrJAXA
+	@description = MCE was launched on July 21, 2012, aboard the H-II Transfer Vehicle KOUNOTORI3 (HTV3 mission) and installed to the EP on August 9, 2012. Onboard five mission payloads listed below are all selected missions thorough deliberation and evaluation by the ISS/JEM Utilization Advisory Committee and JEM-FE sub-committee.
+	@mass = 0.2172
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	JEM NR Science Platform
+@PART[ht2_JEM_NR]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Nanoracks External Platform (NREP)
+	@manufacturer = Nanoracks
+	@description = The Nanoracks External Platform (NREP) provides turnkey communication, power, and operations to hosted payloads mounted on the outside of the International Space Station (ISS).
+	@mass = 0.1448
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	JEM Port
+@PART[ht2_JEM_port]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS JEM Attachment Port
+	@manufacturer = #roMfrJAXA
+	@description = A small docking mechanism for the Japanese Experiment Module's Exposed Facility, designed for attaching scientific payloads.
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	JEM SCI
+@PART[ht2_JEM_SCI]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS JEM SCI (Scientific Data Collector)
+	@manufacturer = #roMfrJAXA
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	JEM SEDA
+@PART[ht2_JEM_SEDA-AP]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS JEM SEDA (Space Environment Data Acquisition Experiment)
+	@manufacturer = #roMfrJAXA
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Quest Pod
+//	Mass: 463kg
+//	Source:		https://space.skyrocket.de/doc_sdat/jam.htm
+//	Source:		http://spacecraftearth.com/#smoothscroll-portfolio-module
+//	Source:		https://www.nasa.gov/pdf/167129main_Systems.pdf
+@PART[ht2_questPod]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Quest Oxygen/Nitrogen Pod
+	@manufacturer = #roMfrBoeing
+	@description = Oxygen/Nitrogen filled resource pods used to maintain total pressure within the cabin. Nitrogen is also required to support on-board experiments and medical equipment.
+	@mass = 0.463
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	//	Remove B9PS tank switching
+	!MODULE[ModuleB9PartSwitch]:HAS[#moduleID[tankSwitch]] {}
+	MODULE
+	{
+		name = ModuleFuelTanks
+		volume = 430
+		basemass = -1
+		type = SM-IV
+	}
+}
+
+
+//	Quest Rack
+@PART[ht2_questRack]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Quest Resource Pod Rack
+	@manufacturer = #roMfrBoeing
+	@description = Oxygen/Nitrogen filled resource pods used to maintain total pressure within the cabin. Nitrogen is also required to support on-board experiments and medical equipment.
+	@mass = 0.005
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+}
+
+
+//	S-Band Antenna
+@PART[ht2_S-band]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS S-Band Antenna
+	@manufacturer = NASA
+	@description = This mast holds a short-range relay antenna via S-Band.
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	!MODULE[ModuleDataTransmitter],* {}
+	MODULE
+	{
+		name = ModuleRealAntenna
+		referenceGain = 2
+		RFBand = S //	Default
+	}
+}
+
+
+//	SGANT Boom Fixed
+@PART[ht2_SGANT_boomFixed]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Antenna Boom (Fixed)
+	@manufacturer = NASA
+	@description = This relatively simple structure provides a mounting point for communications devices.
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	SGANT Boom Swing
+@PART[ht2_SGANT_boomSwing]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Antenna Boom (Rotating)
+	@manufacturer = NASA
+	@description = In order to fold down into a more compact state for launch, this antenna boom arm swings around a slightly unusual axis.
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	SGANT Dish
+@PART[ht2_SGANT_dish]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Relay Antenna
+	@manufacturer = NASA
+	@description = This relatively large relay antenna dish is just right for communications with Geostationary satellite networks.
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	!MODULE[ModuleDataTransmitter],* {}
+	MODULE
+	{
+		name = ModuleRealAntenna
+		referenceGain = 2
+		RFBand = S //	Default
+	}
+}
+
+
+//	SGANT Servo
+@PART[ht2_SGANT_servo]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Pointing Gimbal
+	@manufacturer = NASA
+	@description = This small robotic actuator is ideal for aiming large dish antennas in the right direction.
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	UHF Antenna
+@PART[ht2_UHF_antenna]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Deployable UHF Antenna
+	@manufacturer = NASA
+	@description = Easily confused with a stereo boom microphone, this device is in fact a short-range UHF antenna, ideal for communications to and from the surface of a planet.
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	!MODULE[ModuleDataTransmitter],* {}
+	MODULE
+	{
+		name = ModuleRealAntenna
+		referenceGain = 2
+		RFBand = UHF //	Default
+	}
+}
+
+
+//	WETA
+@PART[ht2_WETA]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Wireless External Transceiver Assembly (WETA)
+	@manufacturer = NASA
+	@description = This mast holds a short-range relay antenna.
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	!MODULE[ModuleDataTransmitter],* {}
+	MODULE
+	{
+		name = ModuleRealAntenna
+		referenceGain = 2
+		RFBand = UHF //	Default
+	}
+}
\ No newline at end of file
diff --git a/GameData/RealismOverhaul/RO_SuggestedMods/HabTech2/RO_HabTech2_modules.cfg b/GameData/RealismOverhaul/RO_SuggestedMods/HabTech2/RO_HabTech2_modules.cfg
index 989f826ab0..61241d81d6 100644
--- a/GameData/RealismOverhaul/RO_SuggestedMods/HabTech2/RO_HabTech2_modules.cfg
+++ b/GameData/RealismOverhaul/RO_SuggestedMods/HabTech2/RO_HabTech2_modules.cfg
@@ -1,404 +1,2083 @@
-//	Common configs for all parts
-@PART[ht2_MPLM|ht2_handrail|ht2_CBM|B10_APASv2|ht2_PMA|ht2_JEM_EF|ht2_moduleColumbus|ht2_moduleCupola|ht2_moduleDestiny|ht2_moduleHarmony|ht2_moduleJEMlogistics|ht2_moduleKibo|ht2_moduleQuest|ht2_moduleUnity|ht2_questRack|ht2_questPod|ht2_MPLM_half|ht2_moduleLabNode]:FOR[RealismOverhaul]
-{
-	%RSSROConfig = True
-	// Multiple rescaleFactor exist on some of the original parts. Remove them first
-	!rescaleFactor,* = DEL
-	%rescaleFactor = 1.81 // Cupola has a different scale, set in later patch
-	@maxTemp = 1073.15
-	@skinMaxTemp = 1073.15
-}
-
-//	Leonardo Permanent Multipurpose Module (PMM)
-//	Diameter: 4.57m (15ft)
-//	Length: 6.6m (22ft)
-//	Mass: 4,082kg (8,999lb)
-//	Source: http://spacecraftearth.com/#smoothscroll-portfolio-module
-
-@PART[ht2_MPLM]:FOR[RealismOverhaul]
-{
-	@mass = 4.082
-	@title = ISS Leonardo PMM
-	@manufacturer = ASI
-	@description = The Leonardo Permanent Multipurpose Module (PMM) is a module of the International Space Station. It was flown into space aboard the Space Shuttle on STS-133 on 24 February 2011 and installed on 1 March. Leonardo is primarily used for storage of spares, supplies and waste on the ISS, which is currently stored in many different places within the space station. The Leonardo PMM was a Multi-Purpose Logistics Module (MPLM) before 2011, but was modified into its current configuration. It was formerly one of three MPLM used for bringing cargo to and from the ISS with the Space Shuttle. The module was named for Italian polymath Leonardo da Vinci.
-
-	MODULE
-	{
-		name = ModuleFuelTanks
-		type = SM-IV
-		basemass = -1
-		volume = 45700 // 2708 cubic feet of pressurized space - the 1095 cubic feet of habitable space = 1613 cubic feet of storage
-	}
-}
-
-@PART[ht2_handrail]:FOR[RealismOverhaul]
-{
-	@title = ISS EVA/Service Handrail
-	@manufacturer = NASA
-	@description = Handrails serve as mobility and stability aids for astronauts during extravehicular activity. Handrails are installed to define a safe path and provide sturdy anchors for the astronauts to use while they are working outside the spacecraft.
-	@mass = 0.001
-}
-
-//	Common Berthing Mechanism
-//	Diameter: 1.8m
-//	Length: 0.4m
-//	Mass: 200kg (440lb)
-//	Source: https://en.wikipedia.org/wiki/Common_Berthing_Mechanism
-@PART[ht2_CBM]:FOR[RealismOverhaul]
-{
-	@mass = 0.2
-	@title = ISS Common Berthing Mechanism
-	@manufacturer = Boeing
-	@description = The common berthing mechanism (CBM) is a berthing mechanism used to connect all non-Russian pressurized modules of the International Space Station. It was developed by Boeing at the Marshall Space Flight Center (MSFC) in Huntsville, Alabama while under contract to the National Aeronautics and Space Administration (NASA).
-
-	@MODULE[ModuleDockingNode]
-	{
-		@nodeType = CBM
-		%acquireForce = 0.5
-		%acquireMinFwdDot = 0.8
-		%acquireminRollDot = -3.40282347E+38
-		%acquireRange = 0.25
-		%acquireTorque = 0.5
-		%captureMaxRvel = 0.1
-		%captureMinFwdDot = 0.998
-		%captureMinRollDot = -3.40282347E+38
-		%captureRange = 0.05
-		%minDistanceToReEngage = 0.25
-		%undockEjectionForce = 0.1
-	}
-}
-
-//	APAS 95
-@PART[B10_APASv2]:FOR[RealismOverhaul]
-{
-	@mass = 0.286
-	@title = APAS 89/95 Active Docking Port
-	@manufacturer = RKK Energia
-	@description = Androgynous Peripheral Attach System developed for the Shuttle-Mir program and ISS. This is the active variant, with a deployable capture ring to align the ports and dampen the impact.
-
-	@MODULE[ModuleDockingNode]
-	{
-		@name = ModuleDockingNode
-		%nodeType = APAS8995
-		%gendered = false
-		%genderFemale = false
-		%acquireForce = 0.5 // 2
-		%acquireMinFwdDot = 0.8 // 0.7
-		%acquireminRollDot = -3.40282347E+38
-		%acquireRange = 0.25 // 0.5
-		%acquireTorque = 0.5 // 2.0
-		%captureMaxRvel = 0.1 // 0.3
-		%captureMinFwdDot = 0.998
-		%captureMinRollDot = -3.40282347E+38
-		%captureRange = 0.05 // 0.06
-		%minDistanceToReEngage = 0.25 // 1.0
-		%undockEjectionForce = 0.1 // 10
-	}
-}
-
-//	Pressurized mating adapter
-//	Width: 19.m - 1.37m
-//	Length: 1.86m (6.1ft)
-//	Mass: 1376kg minus weight for separate APAS port (APAS-95 = 526kg)
-//	Source: https://www.turbosquid.com/3d-models/iss-pressurized-mating-adapter-3d-model/1136389
-@PART[ht2_PMA]:FOR[RealismOverhaul]
-{
-	@mass = 0.850
-	@title = ISS Pressurized Mating Adapter
-	@manufacturer = Boeing
-	@description = The International Space Station (ISS) uses three Pressurized Mating Adapters (PMAs) to interconnect spacecraft and modules with different docking mechanisms. The first two PMAs were launched with the Unity module in 1998 aboard STS-88. The third was launched in 2000 aboard STS-92.
-}
-
-//	JEM Exposed facility
-//	Width: 5m
-//	Length: 5.6m
-//	Mass: 4,100kg (13,450lb)
-//	Source: http://spacecraftearth.com/#smoothscroll-portfolio-module
-@PART[ht2_JEM_EF]:FOR[RealismOverhaul]
-{
-	@mass = 4.1
-	@title = JEM-EF
-	@manufacturer = JAXA
-	@description = The JEM-EF is an external platform for conducting scientific observations, Earth observations, and experiments in an environment exposed to space.
-}
-
-//	ISS Columbus module
-//	Diameter: 4.5m
-//	Length: 7m
-//	Mass: 10,300kg (22,708lb)
-//	Source: http://spacecraftearth.com/#smoothscroll-portfolio-module
-@PART[ht2_moduleColumbus]:FOR[RealismOverhaul]
-{
-	@mass = 10.3
-	@title = ISS Columbus Module
-	@manufacturer = Thales Alenia Space/ EADS
-	@description = Columbus is a science laboratory that is part of the International Space Station (ISS) and is the largest single contribution to the ISS made by the European Space Agency (ESA). Like the Harmony and Tranquility modules, the Columbus laboratory was constructed in Turin, Italy by Rome based Alcatel Alenia Space with respect to structures and thermal control. The functional architecture (including software) of the lab was designed by EADS in Bremen, Germany where it was also integrated before being flown to the Kennedy Space Center (KSC) in Florida in an Airbus Beluga. It was launched aboard Space Shuttle Atlantis on February 7, 2008 on flight STS-122. It is designed for ten years of operation. The module is controlled by the Columbus Control Centre, located at the German Space Operations Centre, part of the German Aerospace Center in Oberpfaffenhofen near Munich, Germany.
-
-	%MODULE[ModuleCommand]
-	{
-		%hasHibernation = True
-		%hibernationMultiplier = 0.01
-		%RESOURCE[ElectricCharge]
-		{
-			%rate = 8.0
-		}
-	}
-
-	MODULE
-	{
-		name = ModuleFuelTanks
-		volume = 25000
-		basemass = -1
-		type = SM-IV
-	}
-}
-
-//	The Cupola
-//	Diameter: 2.95m (9.68ft)
-//	Height: 1.5m (4.9ft)
-//	Mass: 1,880kg (4,145lb)
-//	Source: http://spacecraftearth.com/#smoothscroll-portfolio-module
-@PART[ht2_moduleCupola]:FOR[RealismOverhaul]
-{
-	// scale of Cupola is 2 to match real size. It's too small with 1.81
-	@rescaleFactor = 2
-	@mass = 1.88
-	@category = Utility
-	@title = ISS Cupola
-	@manufacturer = Thales Alenia Space
-	@description = The Cupola is an ESA-built observatory module of the International Space Station (ISS). Its seven windows are used to conduct experiments, dockings and observations of Earth. It was launched aboard Space Shuttle mission STS-130 on 8 February 2010 and attached to the Tranquility (Node 3) module. With the Cupola attached, ISS assembly reached 85 percent completion. The Cupolas 80 cm (31 in) window is the largest ever used in space.
-	@vesselType = Station
-}
-
-//	Destiny module
-//	Diameter: 4.2m (14ft)
-//	Length: 8.4m (28ft)
-//	Mass: 14,515kg (32,000lb)
-//	Source: http://spacecraftearth.com/#smoothscroll-portfolio-module
-@PART[ht2_moduleDestiny]:FOR[RealismOverhaul]
-{
-	@mass = 14.515
-	@title = ISS Destiny
-	@manufacturer = Boeing
-	@description = The Destiny module is the primary operating facility for U.S. research payloads aboard the International Space Station (ISS). It was berthed to the Unity module and activated over a period of five days in February, 2001. Destiny is NASAs first permanent operating orbital research station since Skylab was vacated in February 1974.
-
-	%MODULE[ModuleCommand]
-	{
-		%hasHibernation = True
-		%hibernationMultiplier = 0.01
-		%RESOURCE[ElectricCharge]
-		{
-			%rate = 9.8
-		}
-	}
-
-	MODULE
-	{
-		name = ModuleFuelTanks
-		volume = 8000	// Eight Rack Bays provide 8.2m^3 of storage space usually used for Experiments
-		basemass = -1
-		type = SM-IV
-	}
-}
-
-//	Harmony/Tranquility module
-//	Diameter: 4.4m (14ft)/4.48m (14.7ft)
-//	Length: 7.2m (24ft)/6.71m (22ft)
-//	Mass: 14,288kg (31,500lb)/19,000kg (42,000lb) - adjusted mass of part to be equal.
-//	Source: http://spacecraftearth.com/#smoothscroll-portfolio-module
-//	Source: https://space.skyrocket.de/doc_sdat/node-2.htm
-@PART[ht2_moduleHarmony]:FOR[RealismOverhaul]
-{
-	@mass = 16.644
-	@title = ISS Harmony/Tranquility (Node 2/3)
-	@manufacturer = Thales Alenia Space
-	@description = Harmony/Tranquility, also known as Node 2 and 3 respectively. Node 2 provides a passageway between four station science experiment facilities: the U.S. Destiny Laboratory, the Kibo Japanese Experiment Module, the European Columbus Laboratory and the Centrifuge Accommodation Module. Node 3 contains advanced life support systems and exercise equipment. These systems will recycle waste water for crew use and generate oxygen for the crew to breathe.
-	
-	@CrewCapacity = 4
-
-	MODULE
-	{
-		name = ModuleFuelTanks
-		volume = 39000
-		basemass = -1
-		type = SM-IV
-	}
-}
-
-//	ISS JEM ELM-PS
-//	Diameter: 4.4m (14ft)
-//	Length: 4.2m (13.8ft)
-//	Mass: 8,386kg (18,488lb)
-//	Source: http://spacecraftearth.com/#smoothscroll-portfolio-module
-@PART[ht2_moduleJEMlogistics]:FOR[RealismOverhaul]
-{
-	@mass = 8.386
-	@title = ISS JEM ELM-PS
-	@manufacturer = IHI AEROSPACE
-	@description = The Japanese Experiment Logistics Module, Pressurized Section (ELM-PS), also called the JLP, is a pressurized addition to the PM. The module is a storage facility that provides storage space for experiment payloads, samples and spare items.
-
-	MODULE
-	{
-		name = ModuleFuelTanks
-		volume = 30000
-		basemass = -1
-		type = ServiceModule
-		TANK
-		{
-			name = ElectricCharge
-			amount = 11000
-			maxAmount = 11000
-		}
-	}
-}
-
-//	ISS JEM PM
-//	Diameter: 4.4m (14ft)
-//	Length: 11.2m (36.7ft)
-//	Mass: 15,900kg (35,100lb)
-//	Source: http://spacecraftearth.com/#smoothscroll-portfolio-module
-@PART[ht2_moduleKibo]:FOR[RealismOverhaul]
-{
-	@mass = 15.9
-	@title = ISS Kibo (JEM Pressurized Module)
-	@manufacturer =  Mitsubishi Heavy Industries
-	@description = The Japanese Experiment Module (JEM), also known with the nickname Kibo (Hope), is a Japanese science module for the International Space Station (ISS) developed by JAXA. It is the largest single ISS module. The first two pieces of the module were launched on Space Shuttle missions STS-123 and STS-124. The third and final components were launched on STS-127. The Pressurized Module (PM) is the core component connected to the port hatch of the Node 2 Module. It is cylindrical in shape and contains twenty-three International Standard Payload Racks (ISPRs), ten of which are dedicated to science experiments while the remaining 13 are dedicated to Kibos systems and storage. The racks are placed 6-6-6-5 along the four walls of the module. The end of the JEM-PM has an airlock and two window hatches. The Exposed Facility, Experiment Logistics Module and the Remote Manipulator System all connect to the pressurized module. Kibo is also the location for many of the press conferences that take place on board the station.
-
-	%MODULE[ModuleCommand]
-	{
-		%hasHibernation = True
-		%hibernationMultiplier = 0.01
-		%RESOURCE[ElectricCharge]
-		{
-			%rate = 10.2
-		}
-	}
-
-	MODULE
-	{
-		name = ModuleFuelTanks
-		volume = 85000
-		basemass = -1
-		type = ServiceModule
-		TANK
-		{
-			name = ElectricCharge
-			amount = 15000
-			maxAmount = 15000
-		}
-	}
-}
-
-//	ISS Quest joint airlock
-//	Diameter: 4m (13ft)
-//	Length: 5.5m (18ft)
-//	Mass: 6,064kg (13,369lb) //9,923kg inc 4x N & O2 tanks
-//	Source: https://space.skyrocket.de/doc_sdat/jam.htm
-//	Source: http://spacecraftearth.com/#smoothscroll-portfolio-module
-@PART[ht2_moduleQuest]:FOR[RealismOverhaul]
-{
-	@mass = 6.064
-	@title = ISS Quest Joint Airlock
-	@manufacturer = Boeing
-	@description = The Quest Joint Airlock, previously known as the Joint Airlock Module, is the primary airlock for the International Space Station. Quest was designed to host spacewalks with both Extravehicular Mobility Unit (EMU) spacesuits and Orlan space suits. The airlock was launched on STS-104 on July 14, 2001. Before Quest was attached, Russian spacewalks using Orlan suits could only be done from the Zvezda service module and American spacewalks using EMUs were only possible when a Space Shuttle was docked. The arrival of Pirs docking compartment on September 16, 2001 provided another airlock from which Orlan spacewalks can be conducted.
-	// No Storage space. External tanks are attached to airlock for Nitrogen and Oxygen storage
-}
-
-//	ISS Unity (Node 1)
-//	Diameter: 4.57m (15ft)
-//	Length: 5.47m (17.9ft)
-//	Mass: 11,612kg (25,600lb)
-//	Source: http://spacecraftearth.com/wp-content/uploads/2017/06/Unity-Node-1.jpg
-@PART[ht2_moduleUnity]:FOR[RealismOverhaul]
-{
-	@mass = 11.612
-	@title = ISS Unity (Node 1)
-	@manufacturer = Boeing
-	@description = The Unity connecting module was the first U.S.-built component of the International Space Station. It is cylindrical in shape, with six berthing locations (forward, aft, port, starboard, zenith, and nadir) facilitating connections to other modules. Unity was built for NASA by Boeing in a manufacturing facility at the Marshall Space Flight Center in Huntsville, Alabama. Sometimes referred to as Node 1, Unity was the first of the three connecting modules; the other two are Harmony and Tranquility.
-	@CrewCapacity = 1
-	!RESOURCE,* {}
-	!MODULE[ModuleCommand] {}
-	!MODULE[ModuleFuelTanks],* {}
-
-	MODULE
-	{
-		name = ModuleFuelTanks
-		volume = 10000
-		basemass = -1
-		type = SM-IV
-	}
-}
-
-@PART[ht2_questRack]:FOR[RealismOverhaul]
-{
-	@title = Quest Resource pod rack
-	@manufacturer = Boeing
-	@description = A specially designed rack to hold the Quest resource pod.
-	@mass = 0.005
-}
-
-//	Quest airlock Nitrogen/Oxygen tank
-//	Diameter: ???
-//	Length: ???
-//	Mass: 463kg
-//	Source: https://space.skyrocket.de/doc_sdat/jam.htm
-//	Source: http://spacecraftearth.com/#smoothscroll-portfolio-module
-//	Source: https://www.nasa.gov/pdf/167129main_Systems.pdf
-@PART[ht2_questPod]:FOR[RealismOverhaul]
-{
-	@title = Quest Oxygen/Nitrogen Pod
-	@manufacturer = Boeing
-	@description = Oxygen/Nitrogen filled resource pods used to maintain total pressure within the cabin. Nitrogen is also required to support on-board experiments and medical equipment.
-	@mass = 0.463
-
-	// Remove B9PS tank switching
-	!MODULE[ModuleB9PartSwitch]:HAS[#moduleID[tankSwitch]] {}
-
-	MODULE
-	{
-		name = ModuleFuelTanks
-		volume = 430
-		basemass = -1
-		type = SM-IV
-	}
-}
-
-@PART[ht2_MPLM_half]:FOR[RealismOverhaul]
-{
-	@mass = 2
-	@title = ISS Leonardo Half Module
-
-	MODULE
-	{
-		name = ModuleFuelTanks
-		type = SM-IV
-		basemass = -1
-		volume = 22850 // Presumably half of the MPLM module
-	}
-}
-
-//	HabTech2 LabNode - fictional
-//	Diameter: 4.5m (14.8ft)
-//	Length: 7.65m (25.1ft)
-//	Mass: 18,750kg (41,336lb) - derived from masses of Harmony and Destiny
-@PART[ht2_moduleLabNode]:FOR[RealismOverhaul]
-{
-	@mass = 18.75
-	@title = ISS Laboratory Node
-	@description = This is a fictional ISS module, which combines the capabilities of a laboratory and node passageway into a single module.
-	@manufacturer = Boeing
-
-	MODULE
-	{
-		name = ModuleFuelTanks
-		volume = 46000
-		basemass = -1
-		type = ServiceModule
-		TANK
-		{
-			name = ElectricCharge
-			amount = 10000
-			maxAmount = 10000
-		}
-	}
-}
+//	================================================================================
+//	HabTech2 Modules
+//	================================================================================
+
+
+//	Compact Airlock
+@PART[ht2_airlockCompact]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Compact Airlock
+	@manufacturer = #roMfrBoeing
+	@description = A Small Compact airlock for people, an alternative to the large Quest Airlock.
+	@mass = 1.06
+	@specLevel = concept
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Inline Airlock
+@PART[ht2_airlockInline]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Inline Airlock
+	@manufacturer = #roMfrBoeing
+	@description = A Medium size inline airlock for people, an alternative to the large Quest Airlock.
+	@mass = 2.12
+	@specLevel = concept
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	BEAM
+//	Diameter:	3.23m
+//	Length:		4m
+//	Mass:		1,413kg
+//	Source:		https://www.nasa.gov/international-space-station/bigelow-expandable-activity-module-beam/
+@PART[ht2_BEAM]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Bigelow Expandable Activity Module (BEAM)
+	@manufacturer = Bigelow Aerospace
+	@description = An experimental habitat module which collapses down into a compact cylinder for launch. Launched in 2016, the module demonstrated inflatable habitat structures for use in Crewed Spaceflight.
+	@mass = 1.413
+	@specLevel = operational
+	%skinTempTag = Fiberglass
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Bishop
+//	Diameter:	2.1m
+//	Length:		1.8m
+//	Mass:		1,060kg
+//	Sources:	https://www.eoportal.org/satellite-missions/iss-bishop-airlock#iss-utilization-nanoracks-bishop-airlock-module
+//				https://nanoracks.com/wp-content/uploads/Nanoracks-Bishop-Airlock-IDD.pdf
+@PART[ht2_bishop]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Bishop Airlock
+	@manufacturer = Nanoracks
+	@description = A Small Cargo airlock built by Nanoracks for deploying materials such as CubeSats or Waste. Launched in 2020, the module was deployed and berthed to Node 3 on the ISS.
+	@mass = 1.06
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+}
+
+
+//	Handrail
+@PART[ht2_handrail]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS EVA Handrail
+	@manufacturer = NASA
+	@description = A longitudinal rail designed to allow Astronauts on EVA to grab onto around the outside of a spacecraft. Available in single, double and triple length variants.
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Aluminum
+}
+
+
+//	JEM Arm Mount
+@PART[ht2_JEM_armMount]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS JEM Arm Mount
+	@manufacturer = #roMfrJAXA
+	@description = Mount for the Robotic Arm supporting the Japanese Exposed Facility.
+	@mass = 0.02 // 800kg - 780kg (Arm)
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	JEM Exposed Facility
+//	Diameter:	5m
+//	Length:		5.6m
+//	Mass:		4,100kg
+//	Source:		https://www.eoportal.org/satellite-missions/iss-jem#experiment-logistics-modules
+@PART[ht2_JEM_EF]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Japanese Experiment Module - Exposed Facility
+	@manufacturer = #roMfrJAXA
+	@description = The JEM-EF is an external platform for conducting scientific observations, Earth observations, and experiments in an environment exposed to space.
+	@mass = 4.1
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	JEM EF Port
+@PART[ht2_JEM_EF_port]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS JEM-EF Port
+	@manufacturer = #roMfrJAXA
+	@description = Docking Port for the Japanese Exposed Facility
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	JEM EF Port Passive
+@PART[ht2_JEM_EF_portB]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS JEM-EF Port (Passive)
+	@manufacturer = #roMfrJAXA
+	@description = Docking Port for the Japanese Exposed Facility
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	JEM EF Port Active
+@PART[ht2_JEM_EF_portC]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS JEM-EF Port (Active)
+	@manufacturer = #roMfrJAXA
+	@description = Docking Port for the Japanese Exposed Facility
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Columbus Module
+//	Diameter:	4.5m
+//	Length:		7m
+//	Mass:		10,295kg (@ launch without payload)
+//	Source:		https://www.eoportal.org/satellite-missions/iss-columbus#eop-quick-facts-section
+@PART[ht2_moduleColumbus]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Columbus Module
+	@manufacturer = #roMfrAirbus
+	@description = Columbus is a science laboratory that is part of the International Space Station (ISS) and is the largest single contribution to the ISS made by the European Space Agency (ESA). Like the Harmony and Tranquility modules, the Columbus laboratory was constructed in Turin, Italy by Rome based Alcatel Alenia Space with respect to structures and thermal control. The functional architecture (including software) of the lab was designed by EADS in Bremen, Germany where it was also integrated before being flown to the Kennedy Space Center (KSC) in Florida in an Airbus Beluga. It was launched aboard Space Shuttle Atlantis on February 7, 2008 on flight STS-122. It is designed for ten years of operation. The module is controlled by the Columbus Control Centre, located at the German Space Operations Centre, part of the German Aerospace Center in Oberpfaffenhofen near Munich, Germany.
+	@mass = 10.295
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	%MODULE[ModuleCommand]
+	{
+		%hasHibernation = True
+		%hibernationMultiplier = 0.01
+		%RESOURCE[ElectricCharge]
+		{
+			%rate = 8.0
+		}
+	}
+	MODULE
+	{
+		name = ModuleFuelTanks
+		volume = 25000
+		basemass = -1
+		type = SM-IV
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadTop]]
+	{
+		@SUBTYPE[Bare]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[Bulkhead]
+		{
+			@title = CBM
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Long Columbus Module
+@PART[ht2_moduleColumbusLong]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Freedom Columbus Module
+	@manufacturer = #roMfrAirbus
+	@description = Extended version of the Columbus Module designed for Space Station Freedom, comes with the same equipment and labs that the standard Columbus Module does.
+	@mass = 14.3 // Guess
+	@specLevel = concept
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	%MODULE[ModuleCommand]
+	{
+		%hasHibernation = True
+		%hibernationMultiplier = 0.01
+		%RESOURCE[ElectricCharge]
+		{
+			%rate = 8.0
+		}
+	}
+	MODULE
+	{
+		name = ModuleFuelTanks
+		volume = 50000
+		basemass = -1
+		type = SM-IV
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadTop]]
+	{
+		@SUBTYPE[Bare]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[Bulkhead]
+		{
+			@title = CBM
+		}
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadBottom]]
+	{
+		@SUBTYPE[Bare]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[Bulkhead]
+		{
+			@title = CBM
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Cupola Module
+//	Diameter:	2.95m (9.68ft)
+//	Height:		1.5m (4.9ft)
+//	Mass:		1,805kg (Launch Mass)
+//	Source:		https://www.esa.int/Science_Exploration/Human_and_Robotic_Exploration/Node-3_Cupola/Cupola
+@PART[ht2_moduleCupola]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Cupola Module
+	@manufacturer = Thales Alenia Space
+	@description = The Cupola is an ESA-built observatory module of the International Space Station (ISS). Its seven windows are used to conduct experiments, dockings and observations of Earth. It was launched aboard Space Shuttle mission STS-130 on 8 February 2010 and attached to the Tranquility (Node 3) module. With the Cupola attached, ISS assembly reached 85 percent completion. The Cupolas 80 cm (31 in) window is the largest ever used in space.
+	@mass = 1.805
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Space Station Freedom Cupola
+@PART[ht2_moduleCupolaB]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Freedom Cupola Module
+	@manufacturer = Thales Alenia Space
+	@description = The Cupola is an ESA-built observatory module of Space Station Freedom. Its seven windows are used to conduct experiments, dockings and observations of Earth.
+	@mass = 1.9
+	@specLevel = concept
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Destiny Module
+//	Diameter:	4.5m (14ft)
+//	Length:		8.53m (28ft)
+//	Mass:		14,514kg (32,000lb)
+//	Source:		https://www.nasa.gov/international-space-station/destiny-laboratory-module/
+@PART[ht2_moduleDestiny]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Destiny Module
+	@manufacturer = #roMfrBoeing
+	@description = The Destiny module is the primary operating facility for U.S. research payloads aboard the International Space Station (ISS). It was berthed to the Unity module and activated over a period of five days in February, 2001. Destiny is NASAs first permanent operating orbital research station since Skylab was vacated in February 1974.
+	@mass = 14.514
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	%MODULE[ModuleCommand]
+	{
+		%hasHibernation = True
+		%hibernationMultiplier = 0.01
+		%RESOURCE[ElectricCharge]
+		{
+			%rate = 9.8
+		}
+	}
+	MODULE
+	{
+		name = ModuleFuelTanks
+		volume = 8000	//	Eight Rack Bays provide 8.2m^3 of storage space usually used for Experiments
+		basemass = -1
+		type = SM-IV
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadTop]]
+	{
+		@SUBTYPE[Bare]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[Bulkhead]
+		{
+			@title = CBM
+		}
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadBottom]]
+	{
+		@SUBTYPE[Bare]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[Bulkhead]
+		{
+			@title = CBM
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Freedom Habitat Module
+@PART[ht2_moduleFreedom]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Freedom Long Habitat Module
+	@manufacturer = #roMfrBoeing
+	@description = Habitation module for the cancelled Space Station Freedom.
+	@mass = 20.74 // Guess
+	@specLevel = concept
+	@category = Utility
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE
+	{
+		name = ModuleFuelTanks
+		volume = 11500
+		basemass = -1
+		type = SM-IV
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadTop]]
+	{
+		@SUBTYPE[Bare]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[Bulkhead]
+		{
+			@title = CBM
+		}
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadBottom]]
+	{
+		@SUBTYPE[Bare]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[Bulkhead]
+		{
+			@title = CBM
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Freedom Long Habitat Module
+@PART[ht2_moduleHabLong]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Freedom Habitat Module
+	@manufacturer = #roMfrBoeing
+	@description = Long Habitation module for the cancelled Space Station Freedom.
+	@mass = 14.515 // Guess
+	@specLevel = concept
+	@category = Utility
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE
+	{
+		name = ModuleFuelTanks
+		volume = 8000
+		basemass = -1
+		type = SM-IV
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadTop]]
+	{
+		@SUBTYPE[Bare]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[Bulkhead]
+		{
+			@title = CBM
+		}
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadBottom]]
+	{
+		@SUBTYPE[Bare]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[Bulkhead]
+		{
+			@title = CBM
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Harmony Module
+//	Diameter:	4.4m (14ft)/4.48m (14.7ft)
+//	Length:		7.2m (24ft)/6.71m (22ft)
+//	Mass:		14,288kg (31,500lb)/19,000kg (42,000lb) - adjusted mass of part to be equal.
+//	Source:		https://www.nasa.gov/international-space-station/harmony-module/
+@PART[ht2_moduleHarmony]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Harmony/Tranquility Module (Node 2/3)
+	@manufacturer = Thales Alenia Space
+	@description = Harmony/Tranquility, also known as Node 2 and 3 respectively. Node 2 provides a passageway between four station science experiment facilities: the U.S. Destiny Laboratory, the Kibo Japanese Experiment Module, the European Columbus Laboratory and the Centrifuge Accommodation Module. Node 3 contains advanced life support systems and exercise equipment. These systems will recycle waste water for crew use and generate oxygen for the crew to breathe.
+	@mass = 16.644
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	@CrewCapacity = 4
+	MODULE
+	{
+		name = ModuleFuelTanks
+		volume = 39000
+		basemass = -1
+		type = SM-IV
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadTop]]
+	{
+		@SUBTYPE[Bare]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[Bulkhead]
+		{
+			@title = CBM
+		}
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadBottom]]
+	{
+		@SUBTYPE[Bare]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[Bulkhead]
+		{
+			@title = CBM
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	JEM Logistics Module
+//	Diameter:	4.4m (14ft)
+//	Length:		3.9m (13.8ft)
+//	Mass:		4,200kg
+//	Source:		https://www.eoportal.org/satellite-missions/iss-jem#jemkibo-facilities
+@PART[ht2_moduleJEMlogistics]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Japanese Experiment Module - Logistics Module
+	@manufacturer = #roMfrIHI
+	@description = The Japanese Experiment Logistics Module, Pressurized Section (ELM-PS), also called the JLP, is a pressurized addition to the PM. The module is a storage facility that provides storage space for experiment payloads, samples and spare items.
+	@mass = 4.2
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	@CrewCapacity = 4
+	MODULE
+	{
+		name = ModuleFuelTanks
+		volume = 30000
+		basemass = -1
+		type = SM-IV
+		TANK
+		{
+			name = ElectricCharge
+			amount = 11000
+			maxAmount = 11000
+		}
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadBotton]]
+	{
+		@SUBTYPE[Bare]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[Bulkhead]
+		{
+			@title = CBM
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	JEM Kibo Module
+//	Diameter:	4.4m (14ft)
+//	Length:		11.2m (36.7ft)
+//	Mass:		14,900kg (35,100lb)
+//	Source:		https://www.eoportal.org/satellite-missions/iss-jem#jemkibo-facilities
+@PART[ht2_moduleKibo]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Japanese Experiment Module - Kibo Module
+	@manufacturer = #roMfrMHI
+	@description = The Japanese Experiment Module (JEM), also known with the nickname Kibo (Hope), is a Japanese science module for the International Space Station (ISS) developed by JAXA. It is the largest single ISS module. The first two pieces of the module were launched on Space Shuttle missions STS-123 and STS-124. The third and final components were launched on STS-127. The Pressurized Module (PM) is the core component connected to the port hatch of the Node 2 Module. It is cylindrical in shape and contains twenty-three International Standard Payload Racks (ISPRs), ten of which are dedicated to science experiments while the remaining 13 are dedicated to Kibos systems and storage. The racks are placed 6-6-6-5 along the four walls of the module. The end of the JEM-PM has an airlock and two window hatches. The Exposed Facility, Experiment Logistics Module and the Remote Manipulator System all connect to the pressurized module. Kibo is also the location for many of the press conferences that take place on board the station.
+	@mass = 14.9
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	@CrewCapacity = 4
+	%MODULE[ModuleCommand]
+	{
+		%hasHibernation = True
+		%hibernationMultiplier = 0.01
+		%RESOURCE[ElectricCharge]
+		{
+			%rate = 10.2
+		}
+	}
+	MODULE
+	{
+		name = ModuleFuelTanks
+		volume = 85000
+		basemass = -1
+		type = SM-IV
+		TANK
+		{
+			name = ElectricCharge
+			amount = 15000
+			maxAmount = 15000
+		}
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadBottom]]
+	{
+		@SUBTYPE[Bare]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[Bulkhead]
+		{
+			@title = CBM
+			@NODE[nodeBottom]
+			{
+				@position = 0.0, -1.66444, 0.0
+			}
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Lab Node Module
+//	Diameter:	4.2m (14ft)
+//	Length:		8.4m (28ft)
+//	Mass:		14,514kg (32,000lb)
+//	Source:		https://www.nasa.gov/international-space-station/destiny-laboratory-module/
+//	Notes:		Fictional/Cancelled Module, uses Destiny values.
+@PART[ht2_moduleLabNode]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Lab Node Module
+	@manufacturer = #roMfrBoeing
+	@description = ISS Lab Module with 6 Berthing Nodes.
+	@mass = 14.514
+	@specLevel = concept
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	%MODULE[ModuleCommand]
+	{
+		%hasHibernation = True
+		%hibernationMultiplier = 0.01
+		%RESOURCE[ElectricCharge]
+		{
+			%rate = 9.8
+		}
+	}
+	MODULE
+	{
+		name = ModuleFuelTanks
+		volume = 8000	//	Eight Rack Bays provide 8.2m^3 of storage space usually used for Experiments
+		basemass = -1
+		type = SM-IV
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadTop]]
+	{
+		@SUBTYPE[Bare]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[Bulkhead]
+		{
+			@title = CBM
+		}
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadBottom]]
+	{
+		@SUBTYPE[Bare]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[Bulkhead]
+		{
+			@title = CBM
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Quest Airlock Module
+//	Diameter:	4m (13ft)
+//	Length:		5.5m (18ft)
+//	Mass:		6,064kg (13,369lb) //9,923kg inc 4x N & O2 tanks
+//	Source:		https://space.skyrocket.de/doc_sdat/jam.htm
+//				http://spacecraftearth.com/#smoothscroll-portfolio-module
+@PART[ht2_moduleQuest]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Quest Joint Airlock
+	@manufacturer = #roMfrBoeing
+	@description = The Quest Joint Airlock, previously known as the Joint Airlock Module, is the primary airlock for the International Space Station. Quest was designed to host spacewalks with both Extravehicular Mobility Unit (EMU) spacesuits and Orlan space suits. The airlock was launched on STS-104 on July 14, 2001. Before Quest was attached, Russian spacewalks using Orlan suits could only be done from the Zvezda service module and American spacewalks using EMUs were only possible when a Space Shuttle was docked. The arrival of Pirs docking compartment on September 16, 2001 provided another airlock from which Orlan spacewalks can be conducted.
+	@mass = 6.064
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadBottom]]
+	{
+		@SUBTYPE[Bare]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[Bulkhead]
+		{
+			@title = CBM
+			@NODE[nodeBottom]
+			{
+				@position = 0.0, -0.901667, 0.0
+			}
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Unity Module
+//	Diameter:	4.57m (15ft)
+//	Length:		5.47m (17.9ft)
+//	Mass:		11,612kg (25,600lb) (Includes 2 PMAs, mass subtracted for individual use)
+//	Mass:		8,860kg (Without PMAs)
+//	Source:		https://www.nasa.gov/international-space-station/unity-module/
+@PART[ht2_moduleUnity]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Unity Module (Node 1)
+	@manufacturer = #roMfrBoeing
+	@description = The Unity connecting module was the first U.S.-built component of the International Space Station. It is cylindrical in shape, with six berthing locations (forward, aft, port, starboard, zenith, and nadir) facilitating connections to other modules. Unity was built for NASA by Boeing in a manufacturing facility at the Marshall Space Flight Center in Huntsville, Alabama. Sometimes referred to as Node 1, Unity was the first of the three connecting modules; the other two are Harmony and Tranquility.
+	@mass = 8.86
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	!RESOURCE,* {}
+	!MODULE[ModuleCommand] {}
+	!MODULE[ModuleFuelTanks],* {}
+	MODULE
+	{
+		name = ModuleFuelTanks
+		volume = 10000
+		basemass = -1
+		type = SM-IV
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadTop]]
+	{
+		@SUBTYPE[Bare]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[Bulkhead]
+		{
+			@title = CBM
+		}
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadBottom]]
+	{
+		@SUBTYPE[Bare]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[Bulkhead]
+		{
+			@title = CBM
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	MPLM Half Module
+//	Diameter:	4.5m (14.76ft)
+//	Length:		2.1m (10.85ft)
+//	Mass:		2,219kg (4,892lb)
+//	Source:		https://www.nasa.gov/international-space-station/permanent-multipurpose-module/
+@PART[ht2_MPLM_half]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS MPLM Half Module
+	@manufacturer = #roMfrBoeing
+	@description = Half Size Cargo Module launched via the Space Shuttle, berthed to the Station to extract supplies and equipment for the Space Station. One MPLM was left permenently on the ISS, named Leonardo.
+	@mass = 2.219
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE
+	{
+		name = ModuleFuelTanks
+		type = SM-IV
+		basemass = -1
+		volume = 22850 //	Presumably half of the MPLM module
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadTop]]
+	{
+		@SUBTYPE[Bare]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[Bulkhead]
+		{
+			@title = CBM
+		}
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadBottom]]
+	{
+		@SUBTYPE[Bare]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[Bulkhead]
+		{
+			@title = CBM
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	MPLM Module
+//	Diameter:	4.5m (14.76ft)
+//	Length:		4.2m (21.7ft)
+//	Mass:		4,438kg (9,784lb)
+//	Source:		https://www.nasa.gov/international-space-station/permanent-multipurpose-module/
+@PART[ht2_MPLM]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS MPLM Module
+	@manufacturer = #roMfrBoeing
+	@description = Full Size Cargo Module launched via the Space Shuttle, berthed to the Station to extract supplies and equipment for the Space Station. One MPLM was left permenently on the ISS, named Leonardo.
+	@mass = 4.438
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE
+	{
+		name = ModuleFuelTanks
+		type = SM-IV
+		basemass = -1
+		volume = 45700
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadTop]]
+	{
+		@SUBTYPE[Bare]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[Bulkhead]
+		{
+			@title = CBM
+		}
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadBottom]]
+	{
+		@SUBTYPE[Bare]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[Bulkhead]
+		{
+			@title = CBM
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Freedom Docking Node
+@PART[ht2_orb]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Freedom Docking Node
+	@manufacturer = #roMfrBoeing
+	@description = Docking Node for Space Station Freedom, comes in variants for both APAS/NDS Ports and for CBMs.
+	@mass = 2.7 //	Guess
+	@specLevel = concept
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	%MODULE[ModuleCommand]
+	{
+		%RESOURCE[ElectricCharge]
+		{
+			%rate = 2.0
+		}
+	}
+	MODULE
+	{
+		name = ModuleFuelTanks
+		volume = 2000
+		basemass = -1
+		type = SM-IV
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[node]]
+	{
+		@SUBTYPE[9375]
+		{
+			@title = APAS/NDS
+		}
+		@SUBTYPE[125]
+		{
+			@title = CBM
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Pressurized Mating Adapter
+//	Width:		1.9m - 1.37m
+//	Length:		1.86m (6.1ft)
+//	Mass:		1376kg minus weight for separate APAS port (APAS-95 = 526kg)
+//	Source:		https://www.turbosquid.com/3d-models/iss-pressurized-mating-adapter-3d-model/1136389
+@PART[ht2_PMA]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.7 //	Averaged Value
+	@title = Pressurized Matting Adapter (ISS)
+	@manufacturer = #roMfrBoeing
+	@description = The International Space Station (ISS) uses three Pressurized Mating Adapters (PMAs) to interconnect spacecraft and modules with different docking mechanisms. The first two PMAs were launched with the Unity module in 1998 aboard STS-88. The third was launched in 2000 aboard STS-92.
+	@mass = 0.85
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Straight Alt PMA
+@PART[ht2_PMA_straight]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Pressurized Matting Adapter (Straight)
+	@manufacturer = Axiom Space
+	@description = Straight version of the Pressurized Mating Adapter used on the Axiom Commercial Space Station
+	@mass = 1.25 //	Guess
+	@specLevel = concept
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Short Alt PMA
+@PART[ht2_PMA_short]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Pressurized Matting Adapter (Compact)
+	@manufacturer = Axiom Space
+	@description = Short and Straight version of the Pressurized Mating Adapter used on the Axiom Commercial Space Station
+	@mass = 0.75 //	Guess
+	@specLevel = concept
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	SCRAM
+//	Using Orion CM Stats
+@PART[ht2_SCRAM]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	%rescaleFactor = 1.8
+	@title = SCRAM (Station Crew Return Alternative Module)
+	@mass = 6.230
+	@manufacturer = NASA
+	@description = Provides a safe haven for crew in the likely event of an emergency.
+	@specLevel = concept
+	@maxTemp = 900
+	@skinMaxTemp = 3200 //	Keeps Overheating
+	@emissiveConstant = 0.4
+	@heatConductivity = 1.0
+	@thermalMassModifier = 1.0
+	@skinInternalConductionMult = 0.005
+	@skinMassPerArea = 19.2
+	@skinThermalMassModifier = 1.0
+	@skinSkinConductionMult = 0.005
+	!MODULE[ModuleDataTransmitter],* {}
+	@MODULE[ModuleCommand]
+	{
+		@minimumCrew = 0
+		RESOURCE
+		{
+			name = ElectricCharge
+			rate = 1.895
+		}
+	}
+	!RESOURCE[*],* {}
+	!MODULE[ModuleReactionWheel],* {}
+	MODULE
+	{
+		name = ModuleFuelTanks
+		basemass = -1
+		type = ServiceModule
+		volume = 3000
+		TANK
+		{
+			//	8 batteries at 120 Volt, 30 Ah
+			name = ElectricCharge
+			amount = 103680
+			maxAmount = 103680
+		}
+		TANK
+		{
+			name = Hydrazine
+			amount = 147
+			maxAmount = 147
+		}
+		TANK
+		{
+			name = Helium
+			amount = 1653.7
+			maxAmount = 1653.7
+		}
+	}
+	@MODULE[ModuleRCSFX]
+	{
+		@thrusterPower = 0.8
+		!resourceName = DELETE
+		@resourceFlowMode = STAGE_PRIORITY_FLOW
+		PROPELLANT
+		{
+			name = Hydrazine
+			ratio = 1.0
+		}
+		PROPELLANT
+		{
+			name = Helium
+			ratio = 11.2
+			ignoreForIsp = True
+		}
+		atmosphereCurve
+		{
+			key = 0 240
+			key = 1 100
+			key = 4 0.001
+		}
+	}
+	MODULE
+	{
+		name = AdjustableCoMShifter
+		DescentModeCoM = 0.0, 0.0, 0.2
+	}
+
+	//	Using Orion CM Antennas
+	MODULE
+	{
+		name = ModuleRealAntenna
+		referenceGain = 1.5
+		RFBand = S		//Default to S-band
+	}
+	MODULE
+	{
+		name = ModuleRealAntenna
+		antennaDiameter = 0.8
+		RFBand = K	//Default to K-band
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	SCRAM Chutes
+@PART[ht2_SCRAM_chute]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	@rescaleFactor = 1.8
+	@title = SCRAM Parachute
+	@description = Large Parachute designed to slow you down to a soft splashdown. This part comes with only One Chute.
+	@manufacturer = #roMfrLM
+	@specLevel = concept
+	%skinTempTag = Nomex
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	!MODULE[ModuleParachute],* {}
+	!MODULE:HAS[#name[ModuleDragModifier]],* {}
+	MODULE
+	{
+		name = RealChuteModule
+		caseMass = 0.3498
+		timer = 0
+		mustGoDown = false
+		spareChutes = 1
+		cutSpeed = 0.25
+		PARACHUTE
+		{
+			parachuteName = orion_mainChute_tripleCanopy
+			capName = pack
+			preDeploymentAnimation = mainChute_semiDeploy
+			deploymentAnimation = mainChute_fullyDeploy
+			material = Nylon
+			minIsPressure = False
+			minPressure = 0.01
+			preDeployedDiameter = 16
+			preDeploymentSpeed = 3.0
+			minDeployment = 2895
+			deployedDiameter = 48
+			deploymentSpeed = 5.0
+			deploymentAlt = 2500
+			cutAlt = 0
+		}
+	}
+	MODULE
+	{
+		name = ModuleDragModifier
+		dragCubeName = SEMIDEPLOYED
+		dragModifier = 0.9375
+	}
+	MODULE
+	{
+		name = ModuleDragModifier
+		dragCubeName = DEPLOYED
+		dragModifier = 5
+	}
+}
+@PART[ht2_SCRAM_chute]:AFTER[RealismOverhaul_Materials]
+{
+	@skinMaxTemp = 1533 //	Keeps Overheating
+}
+
+
+//	Generic Hab (4.5m)
+@PART[ht2_size2_hab]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = 4.5m Habitat Module
+	@manufacturer = #roMfrBoeing
+	@mass = 10 // Approx Guess
+	@specLevel = concept
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE
+	{
+		name = ModuleFuelTanks
+		type = SM-IV
+		basemass = -1
+		volume = 25000
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadTop]]
+	{
+		@SUBTYPE[size2]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[size1]
+		{
+			@title = CBM
+		}
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadBottom]]
+	{
+		@SUBTYPE[size2]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[size1]
+		{
+			@title = CBM
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Generic Node (4.5m)
+@PART[ht2_size2_node]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = 4.5m Node Module
+	@manufacturer = #roMfrBoeing
+	@mass = 6.222 // Approx Guess
+	@specLevel = concept
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE
+	{
+		name = ModuleFuelTanks
+		type = SM-IV
+		basemass = -1
+		volume = 5000
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadTop]]
+	{
+		@SUBTYPE[size2]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[size1]
+		{
+			@title = CBM
+		}
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadBottom]]
+	{
+		@SUBTYPE[size2]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[size1]
+		{
+			@title = CBM
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Adapter Module (4.5m-6.3m)
+@PART[ht2_size3_cone]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = 4.5m-6.75m Adapter Module
+	@manufacturer = #roMfrBoeing
+	@mass = 15.5 // Approx Guess
+	@specLevel = concept
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE
+	{
+		name = ModuleFuelTanks
+		type = SM-IV
+		basemass = -1
+		volume = 25000
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadTop]]
+	{
+		@SUBTYPE[size2]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[size1]
+		{
+			@title = CBM
+		}
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadBottom]]
+	{
+		@SUBTYPE[size3]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[size2]
+		{
+			@title = ISS (4.5m)
+		}
+		@SUBTYPE[size1]
+		{
+			@title = CBM
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Hab Module (6.75m)
+@PART[ht2_size3_hab]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = 6.75m Habitat Module
+	@manufacturer = #roMfrBoeing
+	@mass = 18.5 // Approx Guess
+	@specLevel = concept
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE
+	{
+		name = ModuleFuelTanks
+		type = SM-IV
+		basemass = -1
+		volume = 22500
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadTop]]
+	{
+		@SUBTYPE[size3]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[size2]
+		{
+			@title = ISS (4.5m)
+		}
+		@SUBTYPE[size1]
+		{
+			@title = CBM
+		}
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadBottom]]
+	{
+		@SUBTYPE[size3]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[size2]
+		{
+			@title = ISS (4.5m)
+		}
+		@SUBTYPE[size1]
+		{
+			@title = CBM
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Long Hab Module (6.3m)
+@PART[ht2_size3_hab2]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = 6.75m Long Habitat Module
+	@manufacturer = #roMfrBoeing
+	@mass = 35.5 // Approx Guess
+	@specLevel = concept
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE
+	{
+		name = ModuleFuelTanks
+		type = SM-IV
+		basemass = -1
+		volume = 45000
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadTop]]
+	{
+		@SUBTYPE[size3]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[size2]
+		{
+			@title = ISS (4.5m)
+		}
+		@SUBTYPE[size1]
+		{
+			@title = CBM
+		}
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadBottom]]
+	{
+		@SUBTYPE[size3]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[size2]
+		{
+			@title = ISS (4.5m)
+		}
+		@SUBTYPE[size1]
+		{
+			@title = CBM
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Node Module (6.3m)
+@PART[ht2_size3_node]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = 6.75m Node Module
+	@manufacturer = #roMfrBoeing
+	@mass = 15.2 // Approx Guess
+	@specLevel = concept
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE
+	{
+		name = ModuleFuelTanks
+		type = SM-IV
+		basemass = -1
+		volume = 15000
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadTop]]
+	{
+		@SUBTYPE[size3]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[size2]
+		{
+			@title = ISS (4.5m)
+		}
+		@SUBTYPE[size1]
+		{
+			@title = CBM
+		}
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadBottom]]
+	{
+		@SUBTYPE[size3]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[size2]
+		{
+			@title = ISS (4.5m)
+		}
+		@SUBTYPE[size1]
+		{
+			@title = CBM
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Short Hab Module (6.3m)
+@PART[ht2_size3_short]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = 6.3m Short Logistics Module
+	@manufacturer = #roMfrBoeing
+	@mass = 7.8 // Approx Guess
+	@specLevel = concept
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE
+	{
+		name = ModuleFuelTanks
+		type = SM-IV
+		basemass = -1
+		volume = 20000
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadTop]]
+	{
+		@SUBTYPE[size3]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[size2]
+		{
+			@title = ISS (4.5m)
+		}
+		@SUBTYPE[size1]
+		{
+			@title = CBM
+		}
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadBottom]]
+	{
+		@SUBTYPE[size3]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[size2]
+		{
+			@title = ISS (4.5m)
+		}
+		@SUBTYPE[size1]
+		{
+			@title = CBM
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Adapter Module (6.75m-9m)
+@PART[ht2_size4_cone]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = 6.75m-9m Adapter Module
+	@manufacturer = #roMfrBoeing
+	@mass = 21 // Approx Guess
+	@specLevel = concept
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE
+	{
+		name = ModuleFuelTanks
+		type = SM-IV
+		basemass = -1
+		volume = 40000
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadTop]]
+	{
+		@SUBTYPE[size3]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[size2]
+		{
+			@title = ISS (4.5m)
+		}
+		@SUBTYPE[size1]
+		{
+			@title = CBM
+		}
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadBottom]]
+	{
+		@SUBTYPE[size4]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[size3]
+		{
+			@title = 6.75m
+		}
+		@SUBTYPE[size2]
+		{
+			@title = ISS (4.5m)
+		}
+		@SUBTYPE[size1]
+		{
+			@title = CBM
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Habitat Module (9m)
+@PART[ht2_size4_hab]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = 9m Habitat Module
+	@manufacturer = #roMfrBoeing
+	@mass = 22 // Approx Guess
+	@specLevel = concept
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE
+	{
+		name = ModuleFuelTanks
+		type = SM-IV
+		basemass = -1
+		volume = 60000
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadTop]]
+	{
+		@SUBTYPE[size4]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[size3]
+		{
+			@title = 6.75m
+		}
+		@SUBTYPE[size2]
+		{
+			@title = ISS (4.5m)
+		}
+		@SUBTYPE[size1]
+		{
+			@title = CBM
+		}
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadBottom]]
+	{
+		@SUBTYPE[size4]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[size3]
+		{
+			@title = 6.75m
+		}
+		@SUBTYPE[size2]
+		{
+			@title = ISS (4.5m)
+		}
+		@SUBTYPE[size1]
+		{
+			@title = CBM
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Long Habitat Module (9m)
+@PART[ht2_size4_hab2]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = 9m Long Habitat Module
+	@manufacturer = #roMfrBoeing
+	@mass = 40 // Approx Guess
+	@specLevel = concept
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE
+	{
+		name = ModuleFuelTanks
+		type = SM-IV
+		basemass = -1
+		volume = 120000
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadTop]]
+	{
+		@SUBTYPE[size4]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[size3]
+		{
+			@title = 6.75m
+		}
+		@SUBTYPE[size2]
+		{
+			@title = ISS (4.5m)
+		}
+		@SUBTYPE[size1]
+		{
+			@title = CBM
+		}
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadBottom]]
+	{
+		@SUBTYPE[size4]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[size3]
+		{
+			@title = 6.75m
+		}
+		@SUBTYPE[size2]
+		{
+			@title = ISS (4.5m)
+		}
+		@SUBTYPE[size1]
+		{
+			@title = CBM
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Logistics Module (9m)
+@PART[ht2_size4_short]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = 9m Logistics Module
+	@manufacturer = #roMfrBoeing
+	@mass = 22 // Approx Guess
+	@specLevel = concept
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE
+	{
+		name = ModuleFuelTanks
+		type = SM-IV
+		basemass = -1
+		volume = 60000
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadTop]]
+	{
+		@SUBTYPE[size4]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[size3]
+		{
+			@title = 6.75m
+		}
+		@SUBTYPE[size2]
+		{
+			@title = ISS (4.5m)
+		}
+		@SUBTYPE[size1]
+		{
+			@title = CBM
+		}
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadBottom]]
+	{
+		@SUBTYPE[size4]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[size3]
+		{
+			@title = 6.75m
+		}
+		@SUBTYPE[size2]
+		{
+			@title = ISS (4.5m)
+		}
+		@SUBTYPE[size1]
+		{
+			@title = CBM
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Node Module (9m)
+@PART[ht2_size4_node]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = 9m Node Module
+	@manufacturer = #roMfrBoeing
+	@mass = 24 // Approx Guess
+	@specLevel = concept
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE
+	{
+		name = ModuleFuelTanks
+		type = SM-IV
+		basemass = -1
+		volume = 40000
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadTop]]
+	{
+		@SUBTYPE[size4]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[size3]
+		{
+			@title = 6.75m
+		}
+		@SUBTYPE[size2]
+		{
+			@title = ISS (4.5m)
+		}
+		@SUBTYPE[size1]
+		{
+			@title = CBM
+		}
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bulkheadBottom]]
+	{
+		@SUBTYPE[size4]
+		{
+			@title = Flat
+		}
+		@SUBTYPE[size3]
+		{
+			@title = 6.75m
+		}
+		@SUBTYPE[size2]
+		{
+			@title = ISS (4.5m)
+		}
+		@SUBTYPE[size1]
+		{
+			@title = CBM
+		}
+	}
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Toolbox 1
+@PART[ht2_toolBox1]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	%ROCargoConfig = True
+	@title = ISS EVA Toolbox 1
+	@manufacturer = #roMfrBoeing
+	@description = Toolbox for Astronauts on EVA around the International Space Station.
+	@mass = 0.1
+	@specLevel = concept
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
+
+
+//	Toolbox 2
+@PART[ht2_toolBox2]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	%ROCargoConfig = True
+	@title = ISS EVA Toolbox 2
+	@manufacturer = #roMfrBoeing
+	@description = Toolbox for Astronauts on EVA around the International Space Station.
+	@mass = 0.05
+	@specLevel = concept
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%skinInsulationTag = True
+	MODULE:NEEDS[ConnectedLivingSpace]
+	{
+		name = ModuleConnectedLivingSpace
+		passable = True
+		passableWhenSurfaceAttached = true
+		surfaceAttachmentsPassable = true
+	}
+}
\ No newline at end of file
diff --git a/GameData/RealismOverhaul/RO_SuggestedMods/HabTech2/RO_HabTech2_truss.cfg b/GameData/RealismOverhaul/RO_SuggestedMods/HabTech2/RO_HabTech2_truss.cfg
index beccb8a14d..23df26a5fa 100644
--- a/GameData/RealismOverhaul/RO_SuggestedMods/HabTech2/RO_HabTech2_truss.cfg
+++ b/GameData/RealismOverhaul/RO_SuggestedMods/HabTech2/RO_HabTech2_truss.cfg
@@ -1,184 +1,923 @@
-//	Common configs for all parts
-@PART[ht2_solarArray_duo|ht2_truss_S0|ht2_truss_S1|ht2_radiatorTriple|ht2_radialTrussPort|ht2_truss_S2|ht2_truss_Z1|ht2_truss_Z1_v2|ht2_trussPort]:FOR[RealismOverhaul]
-{
-	%RSSROConfig = True
-	// Multiple rescaleFactor exist on some of the original parts. Remove them first
-	!rescaleFactor,* = DEL
-	%rescaleFactor = 1.81 // Cupola has a different scale, set in later patch
-	@maxTemp = 1073.15
-	@skinMaxTemp = 1073.15
-}
-
-//	ISS Solar arrays & trusses (P4/S4 - P6/S6)
-//	(P3/S3 truss is a separate part in HT2 so isn't factored into the solar array config)
-//	Diameter: 10.7m (35ft)
-//	Length: 73.2m (240.2ft)
-//	Mass: 15,900kg //15900kg (#P3/4); 16183kg (#S3/4) split the difference for the mass of the two S3/P3 trusses
-//	Source: https://space.skyrocket.de/doc_sdat/its-s3-4.htm
-//	Source: http://spacecraftearth.com/#smoothscroll-portfolio-module
-@PART[ht2_solarArray_duo]:FOR[RealismOverhaul]
-{
-	@mass = 15.900
-	@title = ISS P4-P6/S4-S6
-	@manufacturer = Boeing
-	@description = The International Space Station's main source of energy is from three of the four large U.S.-made photovoltaic arrays currently on the station, sometimes referred to as the Solar Array Wings (SAW). The first pair of arrays are attached to the P6 truss segment, which was launched and installed on top of Z1 in late 2000 during STS-97. The P6 segment was relocated to its final position, bolted to the P5 truss segment, in November 2007 during STS-120. The second pair of arrays was launched and installed in September 2006 during STS-115, but they didn't provide electricity until STS-116 in December 2006 when the station got an electrical rewiring. A third pair of arrays was installed during STS-117 in June 2007. A final pair arrived mid March 2009 on STS-119. More solar power was to have been available via the Russian-built Science Power Platform, but it was canceled.
-
-	// Area gives each module 30 kW at tech level 6
-	SolarConfig
-	{
-		area = 113.21
-		level = 7
-	}
-
-	// Disable SolarConfig from changing the dummy module for solar tracking
-	@MODULE[ModuleDeployableSolarPanel]:HAS[#pivotName[SARJ]]
-	{
-		@chargeRate = 0.000001
-		realismOverhaulSolarIgnore = true
-	}
-
-	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[topMount]]
-	{
-		// Average of S5/P5 truss
-		@SUBTYPE[S5]
-		{
-			%addedMass = 1.841
-		}
-	}
-
-	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[bottomMount]]
-	{
-		@SUBTYPE[SARJ]
-		{
-			%addedMass = 1.134
-		}
-	}
-}
-
-//	ISS S0 truss
-//	Diameter: 4.6m
-//	Length: 13.4m
-//	Mass: 13,970kg (30,800lb)
-//	Source: http://spacecraftearth.com/#smoothscroll-portfolio-module
-@PART[ht2_truss_S0]:FOR[RealismOverhaul]
-{
-	@mass = 13.970
-	@title = ISS S0 Truss Segment
-	@manufacturer = Boeing
-	@description = The S0 truss, (also called the Center Integrated Truss Assembly Starboard 0 Truss) forms the center backbone of the Space Station. It was attached on the top of the Destiny Laboratory Module during STS-110 in April 2002. S0 is used to route power to the pressurized station modules and conduct heat away from the modules to the S1 and P1 Trusses.
-
-	@RESOURCE[ElectricCharge]
-	{
-		@name = ElectricCharge
-		%amount = 3000
-		%maxAmount = 3000
-	}
-}
-
-//	ISS S1/P1 truss
-//	Diameter: 4.6m
-//	Length: 13.7m
-//	Mass: 9,124kg // 12,524kg (27,611lb) inc triple HRS (separate part)
-//	Source: https://space.skyrocket.de/doc_sdat/its-s1.htm
-@PART[ht2_truss_S1]:FOR[RealismOverhaul]
-{
-	@mass = 9.124
-	@title = ISS S1/P1 Truss Segment
-	@manufacturer = Boeing
-	@description = The P1 and S1 trusses (also called the Port and Starboard Side Thermal Radiator Trusses) are attached to the S0 truss, and contain carts to transport the Canadarm2 and astronauts to worksites along the space station. They each flow 290 kg (637 lb) of anhydrous ammonia through three heat rejection radiators. The S1 truss was launched on STS-112 in October 2002 and the P1 truss was launched on STS-113 in November 2002.
-
-	@RESOURCE[ElectricCharge]
-	{
-		@name = ElectricCharge
-		%amount = 2500
-		%maxAmount = 2500
-	}
-}
-
-//	ISS Triple HRS
-//	Diameter: ?
-//	Length: 22.86m (75ft)
-//	Mass: 3,400kg (7496lb)
-//	Source: http://www.defense-aerospace.com/article-view/release/12155/lockheed-hrs-radiators-on-board-atlantis-(oct.-10).html
-@PART[ht2_radiatorTriple]:FOR[RealismOverhaul]
-{
-	@mass = 3.4
-	@title = ISS Triple HRS Radiators
-	@manufacturer = Lockheed Martin
-	@description = The three HRS radiators on S1 weigh approximately 7,500 pounds, which is almost 30 percent of the payload on the Space Shuttle Atlantis.
-	%breakingForce = 200
-	%breakingTorque = 200
-	%fuelCrossFeed = False
-	%radiatorHeadroom = 0.29 // 0.2702 sets the limit to 17C, or 290K
-
-	@MODULE[ModuleActiveRadiator]
-	{
-		@maxEnergyTransfer = 1750
-		@overcoolFactor = 0.0186367
-
-		@RESOURCE[ElectricCharge]
-		{
-			@rate = 1.545
-		}
-	}
-}
-
-//	Radial truss port to secure S0 to Destiny module
-@PART[ht2_radialTrussPort]:FOR[RealismOverhaul]
-{
-	@title = ISS S0 Radial Truss Connector
-	@manufacturer = Boeing
-	@description = A radially-attachable mechanism designed for connecting the S0 truss to the ISS.
-}
-
-//	P3/S3 truss
-//	Separate part in HT2, Originally apart of P4/S4.
-//	Mass: 141.5kg
-@PART[ht2_truss_S2]:FOR[RealismOverhaul]
-{
-	@mass = 0.1415
-	@title = ISS P3/S3 Truss Segment
-	@manufacturer = Boeing
-	@description = The P3/S3 primary structure is made of a hexagonal shaped aluminum structure and includes four bulkheads and six longerons. Used to connect P4/S4, don't forget your dockable truss port!
-}
-
-//	ITS-Z1
-//	Diameter: 4.2m (13.8ft)
-//	Length: 4.9m (16ft)
-//	Mass: 8,755kg (19,300lb)
-//	Source: http://spacecraftearth.com/#smoothscroll-portfolio-module
-//	Source: https://space.skyrocket.de/doc_sdat/its-z1.htm
-@PART[ht2_truss_Z1|ht2_truss_Z1_v2]:FOR[RealismOverhaul]
-{
-	@mass = 8.755
-	@title = ISS Z1 Truss Segment
-	@manufacturer = Boeing
-	@description = The first truss piece, the Z1 truss, launched aboard STS-92 in October 2000. It contains the control moment gyroscope (CMG) assemblies, electrical wiring, communications equipment, and two plasma contactors designed to neutralize the static electrical charge of the space station. Another objective of the Z1 truss was to serve as a temporary mounting position for the "P6 truss and solar array" until its relocation to the end of the P5 truss during STS-120. Though not a part of the main truss, the Z1 truss was the first permanent lattice-work structure for the ISS, very much like a girder, setting the stage for the future addition of the stations major trusses or backbones.
-
-	@MODULE[ModuleReactionWheel]
-	{
-		@PitchTorque = 5
-		@YawTorque = 5
-		@RollTorque = 5
-
-		@RESOURCE[ElectricCharge]
-		{
-			@rate = 0.8
-		}
-	}
-
-	@RESOURCE[ElectricCharge]
-	{
-		@amount = 1000
-		@maxAmount = 1000
-	}
-}
-
-//	Part switchable truss docking port for all ITS and docking to the radial truss connector on the top of Destiny.
-@PART[ht2_trussPort]:FOR[RealismOverhaul]
-{
-	@mass = 0.05
-	@title = ISS Truss Docking Port
-	@manufacturer = Boeing
-	@description = Docking port to connect the truss segments for the Integrated Truss Structure which contains the large solar arrays and radiators for the International Space Station.
-}
+//	================================================================================
+//	HabTech2 Truss
+//	================================================================================
+
+
+//	AMS
+@PART[ht2_AMS]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Alpha Magnetic Spectrometer Experiment (AMS)
+	@manufacturer = NASA
+	@description = An extremely sensitive science experiment designed to detect charged particle events that would otherwise be obscured by Earth's atmosphere.
+	@mass = 6.717
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	ATA
+@PART[ht2_ATA]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS ATA Multipurpose Tank Assembly
+	@manufacturer = NASA
+	@description = A radially attachable storage tank.
+	@mass = 0.06
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	!MODULE[ModuleB9PartSwitch]:HAS[#moduleID[tankSwitch]] {}
+	MODULE
+	{
+		name = ModuleFuelTanks
+		volume = 237
+		basemass = -1
+		type = SM-IV
+	}
+}
+
+
+//	Battery
+//	Source: https://ntrs.nasa.gov/api/citations/20200000004/downloads/20200000004.pdf
+@PART[ht2_battery]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Radial Battery
+	@manufacturer = NASA
+	@description = External battery pack for the ISS, placed on the Truss structure
+	@mass = 0.17
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	@RESOURCE[ElectricCharge]
+	{
+		@amount = 5000
+		@maxAmount = 5000
+	}
+}
+
+
+//	Bipod Strut
+@PART[ht2_bipod_strut]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	@title = ISS Bipod Strut
+	@manufacturer = NASA
+	@description = Bipod Strut for the S0 Truss segment.
+	@mass = 0.01
+	%skinTempTag = Aluminum
+	%internalTempTag = Aluminum
+}
+
+
+//	Reaction Wheels
+//	Source: https://ntrs.nasa.gov/api/citations/20100021932/downloads/20100021932.pdf
+@PART[ht2_CMG]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Control Moment Gryo
+	@manufacturer = NASA
+	@description = Individual Reaction Wheel for the International Space Station.
+	@mass = 0.1
+	@specLevel = operational
+	%skinTempTag = Steel
+	%internalTempTag = Instruments
+	%reactionWheelPowerDraw = 0.5
+	%reactionWheelMode = CMG
+}
+
+
+//	Freedom Fuel Module
+@PART[ht2_fuelModule]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Freedom Truss Fuel Module
+	@manufacturer = NASA
+	@description = Propellant Tank for the Space Station Freedom/ISS Truss
+	@mass = 1.5
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Aluminum
+	!RESOURCE[*],* {}
+	MODULE
+	{
+		name = ModuleFuelTanks
+		volume = 4500 // 6 Identical Cylindrical Tanks
+		type = Tank-Sep-AlCu-HP
+		basemass = -1
+	}
+}
+
+
+//	iROSA Solar Array
+@PART[ht2_iROSA]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	%ROCargoConfig = True // Supposed to be a Cargo Part?
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = iROSA Solar Array
+	@manufacturer = NASA
+	@description = Roll Out Solar Array meant to supplement power to the ISS with the aging existing solar arrays. Launched and Delivered on a SpaceX Cargo Dragon 2.
+	@mass = 0.325
+	@specLevel = operational
+	%skinTempTag = Solar
+	%internalTempTag = Instruments
+	@MODULE[ModuleDeployableSolarPanel]
+	{
+		@chargeRate = 20
+	}
+}
+
+
+// ================================================================================
+// Integrated Truss Structure
+// ================================================================================
+
+
+//	ITS Adapter
+@PART[ht2_ITS_adapter]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Integrated Truss Structure Adapter
+	@manufacturer = #roMfrBoeing
+	@description = An enormous structural truss section. Adapts from a hexagonal to a semi-hexagonal profile.
+	@mass = 1.2
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	ITS Half
+@PART[ht2_ITS_half_short]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Integrated Truss Structure Half Section
+	@manufacturer = #roMfrBoeing
+	@description = An enormous structural truss section. Semi-hexagonal profile.
+	@mass = 1
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	ITS Hex Half
+@PART[ht2_ITS_hex_half]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Integrated Truss Structure Hexagonal Half Section
+	@manufacturer = #roMfrBoeing
+	@description = An enormous structural truss section. Semi-hexagonal profile.
+	@mass = 0.6
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	ITS Hex
+@PART[ht2_ITS_hex]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Integrated Truss Structure Hexagonal Section
+	@manufacturer = #roMfrBoeing
+	@description = An enormous structural truss section. Hexagonal profile..
+	@mass = 2.5
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	S0 Truss
+//	Diameter:	4.6m
+//	Length:		13.4m
+//	Mass:		13,970kg (30,800lb)
+//	Source:		http://spacecraftearth.com/#smoothscroll-portfolio-module
+@PART[ht2_ITS_S0]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS S0 Truss Segment
+	@manufacturer = #roMfrBoeing
+	@description = The S0 truss, (also called the Center Integrated Truss Assembly Starboard 0 Truss) forms the center backbone of the Space Station. It was attached on the top of the Destiny Laboratory Module during STS-110 in April 2002. S0 is used to route power to the pressurized station modules and conduct heat away from the modules to the S1 and P1 Trusses.
+	@mass = 13.97
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	S1/P1 Truss
+//	Diameter:	4.6m
+//	Length:		13.7m
+//	Mass:		9,124kg
+//	Source:		https://space.skyrocket.de/doc_sdat/its-s1.htm
+@PART[ht2_ITS_S1]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS S1/P1 Truss Segment
+	@manufacturer = #roMfrBoeing
+	@description = The P1 and S1 trusses (also called the Port and Starboard Side Thermal Radiator Trusses) are attached to the S0 truss, and contain carts to transport the Canadarm2 and astronauts to worksites along the space station. They each flow 290 kg (637 lb) of anhydrous ammonia through three heat rejection radiators. The S1 truss was launched on STS-112 in October 2002 and the P1 truss was launched on STS-113 in November 2002.
+	@mass = 9.124
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	S3/P3 Truss
+//	Mass:		141.5kg
+@PART[ht2_ITS_truss01]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS P3/S3 Truss Segment
+	@manufacturer = #roMfrBoeing
+	@title = ISS P3/S3 Truss Segment
+	@mass = 0.1415
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Mobile Base Structure
+@PART[ht2_MBS]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Mobile Base Structure
+	@manufacturer = #roMfrBoeing
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Mobile Transporter Unit
+@PART[ht2_MT]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Mobile Transporter Unit
+	@manufacturer = #roMfrBoeing
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	MTS Adapter
+@PART[ht2_MTS]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Truss Connection Mechanism
+	@manufacturer = #roMfrBoeing
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	MTS Adapter Angled
+@PART[ht2_MTS_adapter]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Truss Connection Mechanism (Angled)
+	@manufacturer = #roMfrBoeing
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	P4 Solar Array
+//	Diameter:	10.7m (35ft)
+//	Length:		73.2m (240.2ft)
+//	Mass:		15,900kg //15900kg (#P3/4); 16183kg (#S3/4) split the difference for the mass of the two S3/P3 trusses
+//	Source:		https://space.skyrocket.de/doc_sdat/its-s3-4.htm
+//	Source:		http://spacecraftearth.com/#smoothscroll-portfolio-module
+@PART[ht2_P3_SAW]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS P4/S4 Solar Array
+	@manufacturer = #roMfrBoeing
+	@description = The International Space Station's main source of energy is from three of the four large U.S.-made photovoltaic arrays currently on the station, sometimes referred to as the Solar Array Wings (SAW). The first pair of arrays are attached to the P6 truss segment, which was launched and installed on top of Z1 in late 2000 during STS-97. The P6 segment was relocated to its final position, bolted to the P5 truss segment, in November 2007 during STS-120. The second pair of arrays was launched and installed in September 2006 during STS-115, but they didn't provide electricity until STS-116 in December 2006 when the station got an electrical rewiring. A third pair of arrays was installed during STS-117 in June 2007. A final pair arrived mid March 2009 on STS-119. More solar power was to have been available via the Russian-built Science Power Platform, but it was canceled.
+	@mass = 15.900
+	@specLevel = operational
+	%skinTempTag = Solar
+	%internalTempTag = Instruments
+	@MODULE[ModuleDeployableSolarPanel]:HAS[#raycastTransformName[suncatcherA]]
+	{
+		@chargeRate = 30 // 240kW / 8 Arrays
+	}
+	@MODULE[ModuleDeployableSolarPanel]:HAS[#raycastTransformName[suncatcher002]]
+	{
+		@chargeRate = 30 // 240kW / 8 Arrays
+	}
+}
+
+
+//	P6 Solar Array
+@PART[ht2_P6_SAW]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS P6 Solar Array
+	@manufacturer = #roMfrBoeing
+	@description = The International Space Station's main source of energy is from three of the four large U.S.-made photovoltaic arrays currently on the station, sometimes referred to as the Solar Array Wings (SAW). The first pair of arrays are attached to the P6 truss segment, which was launched and installed on top of Z1 in late 2000 during STS-97. The P6 segment was relocated to its final position, bolted to the P5 truss segment, in November 2007 during STS-120. The second pair of arrays was launched and installed in September 2006 during STS-115, but they didn't provide electricity until STS-116 in December 2006 when the station got an electrical rewiring. A third pair of arrays was installed during STS-117 in June 2007. A final pair arrived mid March 2009 on STS-119. More solar power was to have been available via the Russian-built Science Power Platform, but it was canceled.
+	@mass = 15.900
+	@specLevel = operational
+	%skinTempTag = Solar
+	%internalTempTag = Instruments
+	@MODULE[ModuleDeployableSolarPanel]:HAS[#raycastTransformName[suncatcherA]]
+	{
+		@chargeRate = 30 // 240kW / 8 Arrays
+	}
+	@MODULE[ModuleDeployableSolarPanel]:HAS[#raycastTransformName[suncatcher002]]
+	{
+		@chargeRate = 30 // 240kW / 8 Arrays
+	}
+}
+
+
+//	S6 Solar Array
+@PART[ht2_S6_SAW]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS S6 Solar Array
+	@manufacturer = #roMfrBoeing
+	@description = The International Space Station's main source of energy is from three of the four large U.S.-made photovoltaic arrays currently on the station, sometimes referred to as the Solar Array Wings (SAW). The first pair of arrays are attached to the P6 truss segment, which was launched and installed on top of Z1 in late 2000 during STS-97. The P6 segment was relocated to its final position, bolted to the P5 truss segment, in November 2007 during STS-120. The second pair of arrays was launched and installed in September 2006 during STS-115, but they didn't provide electricity until STS-116 in December 2006 when the station got an electrical rewiring. A third pair of arrays was installed during STS-117 in June 2007. A final pair arrived mid March 2009 on STS-119. More solar power was to have been available via the Russian-built Science Power Platform, but it was canceled.
+	@mass = 15.900
+	@specLevel = operational
+	%skinTempTag = Solar
+	%internalTempTag = Instruments
+	@MODULE[ModuleDeployableSolarPanel]:HAS[#raycastTransformName[suncatcherA]]
+	{
+		@chargeRate = 30 // 240kW / 8 Arrays
+	}
+	@MODULE[ModuleDeployableSolarPanel]:HAS[#raycastTransformName[suncatcher002]]
+	{
+		@chargeRate = 30 // 240kW / 8 Arrays
+	}
+}
+
+
+//	Prop Module
+@PART[ht2_propModule]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Truss Propellant Module
+	@manufacturer = NASA
+	@description = Propellant Tank for the Space Station Freedom/ISS Truss
+	@mass = 1.5
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Aluminum
+	!RESOURCE[*],* {}
+	MODULE
+	{
+		name = ModuleFuelTanks
+		volume = 4500 // 6 Identical Cylindrical Tanks
+		type = Tank-Sep-AlCu-HP
+		basemass = -1
+	}
+	%useRcsConfig = RCSBlock
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%RcsNozzles = 20
+}
+
+
+//	Radiator Single
+@PART[ht2_radiatorSingle]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Single HRS Radiator
+	@manufacturer = #roMfrLM
+	@mass = 1.133
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%breakingForce = 200
+	%breakingTorque = 200
+	%fuelCrossFeed = False
+	%radiatorHeadroom = 0.29 // 0.2702 sets the limit to 17C, or 290K
+	@MODULE[ModuleActiveRadiator]
+	{
+		@maxEnergyTransfer = 583.33
+		@overcoolFactor = 0.0186367
+		@RESOURCE[ElectricCharge]
+		{
+			@rate = 0.515
+		}
+	}
+}
+
+
+//	Radiator Triple
+//	Length:		22.86m (75ft)
+//	Mass:		3,400kg (7496lb)
+//	Source:		http://www.defense-aerospace.com/article-view/release/12155/lockheed-hrs-radiators-on-board-atlantis-(oct.-10).html
+@PART[ht2_radiatorTriple_v2]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Triple HRS Radiators
+	@manufacturer = #roMfrLM
+	@description = The three HRS radiators on S1 weigh approximately 7,500 pounds, which is almost 30 percent of the payload on the Space Shuttle Atlantis.
+	@mass = 3.4
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%breakingForce = 200
+	%breakingTorque = 200
+	%fuelCrossFeed = False
+	%radiatorHeadroom = 0.29 // 0.2702 sets the limit to 17C, or 290K
+	@MODULE[ModuleActiveRadiator]
+	{
+		@maxEnergyTransfer = 1750
+		@overcoolFactor = 0.0186367
+		@RESOURCE[ElectricCharge]
+		{
+			@rate = 1.545
+		}
+	}
+}
+
+
+//	RCS 1
+@PART[ht2_rcs_1]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Heavy Duty RCS Block 1
+	@manufacturer = #roMfrAerojetRocketdyne
+	@specLevel = concept
+	%useRcsConfig = RCSBlock
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%RcsNozzles = 4
+}
+
+
+//	RCS 1a
+@PART[ht2_rcs_1a]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Heavy Duty Angled RCS Block 1
+	@manufacturer = #roMfrAerojetRocketdyne
+	@specLevel = concept
+	%useRcsConfig = RCSBlock
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%RcsNozzles = 4
+}
+
+
+//	RCS 2
+@PART[ht2_rcs_2]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Heavy Duty RCS Block 2
+	@manufacturer = #roMfrAerojetRocketdyne
+	@specLevel = concept
+	%useRcsConfig = RCSBlock
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%RcsNozzles = 8
+}
+
+
+//	RCS 2a
+@PART[ht2_rcs_2a]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Heavy Duty Angled RCS Block 2
+	@manufacturer = #roMfrAerojetRocketdyne
+	@specLevel = concept
+	%useRcsConfig = RCSBlock
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%RcsNozzles = 8
+}
+
+
+//	RCS 3
+@PART[ht2_rcs_3]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Heavy Duty RCS Block 3
+	@manufacturer = #roMfrAerojetRocketdyne
+	@specLevel = concept
+	%useRcsConfig = RCSBlock
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%RcsNozzles = 12
+}
+
+
+//	RCS 3a
+@PART[ht2_rcs_3a]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Heavy Duty Angled RCS Block 3
+	@manufacturer = #roMfrAerojetRocketdyne
+	@specLevel = concept
+	%useRcsConfig = RCSBlock
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%RcsNozzles = 12
+}
+
+
+//	RCS 3b
+@PART[ht2_rcs_3b]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Heavy Duty RCS Cluster
+	@manufacturer = #roMfrAerojetRocketdyne
+	@specLevel = concept
+	%useRcsConfig = RCSBlock
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%RcsNozzles = 12
+}
+
+
+//	RCS 4
+@PART[ht2_rcs_4]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Heavy Duty RCS Block 4
+	@manufacturer = #roMfrAerojetRocketdyne
+	@specLevel = concept
+	%useRcsConfig = RCSBlock
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%RcsNozzles = 16
+}
+
+
+//	RCS 4a
+@PART[ht2_rcs_4a]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Heavy Duty Angled RCS Block 4
+	@manufacturer = #roMfrAerojetRocketdyne
+	@specLevel = concept
+	%useRcsConfig = RCSBlock
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%RcsNozzles = 16
+}
+
+
+//	RCS 4b
+@PART[ht2_rcs_4b]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Heavy Duty Angled RCS Block 5
+	@manufacturer = #roMfrAerojetRocketdyne
+	@specLevel = concept
+	%useRcsConfig = RCSBlock
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%RcsNozzles = 16
+}
+
+
+//	Large Solar Array
+@PART[ht2_SAW_v2]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Solar Array
+	@manufacturer = #roMfrBoeing
+	@description = Individual Large Solar Array for the International Space Station.
+	@specLevel = operational
+	@mass = 1.6
+	%skinTempTag = Solar
+	%internalTempTag = Instruments
+	@RESOURCE[ElectricCharge]
+	{
+		@amount = 3000
+		@maxAmount = 3000
+	}
+	@MODULE[ModuleDeployableSolarPanel]
+	{
+		@chargeRate = 30 // 240kW / 8 Arrays
+	}
+}
+
+
+//	Half Length Solar Array
+@PART[ht2_SAW_half]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Half Length Solar Array
+	@manufacturer = #roMfrBoeing
+	@description = Individual Half Length Solar Array for the International Space Station.
+	@mass = 1 // Half Mass Array + increase for same mounting hardware
+	@specLevel = operational
+	%skinTempTag = Solar
+	%internalTempTag = Instruments
+	@RESOURCE[ElectricCharge]
+	{
+		@amount = 1500
+		@maxAmount = 1500
+	}
+	@MODULE[ModuleDeployableSolarPanel]
+	{
+		@chargeRate = 15 // (240kW / 8 Arrays)/2
+	}
+}
+
+
+//	SAW Radiator
+@PART[ht2_SAW_radiator]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Small Radiator
+	@manufacturer = #roMfrBoeing
+	@description = Individual small Radiator for the International Space Station.
+	@mass = 1.133
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+	%breakingForce = 200
+	%breakingTorque = 200
+	%fuelCrossFeed = False
+	%radiatorHeadroom = 0.29 // 0.2702 sets the limit to 17C, or 290K
+	@MODULE[ModuleActiveRadiator]
+	{
+		@maxEnergyTransfer = 291.665
+		@overcoolFactor = 0.0186367
+		@RESOURCE[ElectricCharge]
+		{
+			@rate = 0.2575
+		}
+	}
+	@MODULE[ModuleB9PartSwitch]:HAS[#moduleID[length]]
+	{
+		@SUBTYPE[8]
+		{
+			@MODULE:HAS[#IDENTIFIER[ModuleActiveRadiator]]
+			{
+				@DATA
+				{
+					@maxEnergyTransfer = 291.665
+					@RESOURCE[ElectricCharge]
+					{
+						@rate = 0.2575
+					}
+				}
+			}
+		}
+		@SUBTYPE[6]
+		{
+			@addedMass = -0.25
+			@MODULE:HAS[#IDENTIFIER[ModuleActiveRadiator]]
+			{
+				@DATA
+				{
+					@maxEnergyTransfer = 218.74875
+					@RESOURCE[ElectricCharge]
+					{
+						@rate = 0.193125
+					}
+				}
+			}
+		}
+		@SUBTYPE[4]
+		{
+			@addedMass = -0.5
+			@MODULE:HAS[#IDENTIFIER[ModuleActiveRadiator]]
+			{
+				@DATA
+				{
+					@maxEnergyTransfer = 145.8325
+					@RESOURCE[ElectricCharge]
+					{
+						@rate = 0.12875
+					}
+				}
+			}
+		}
+		@SUBTYPE[2]
+		{
+			@addedMass = -0.75
+			@MODULE:HAS[#IDENTIFIER[ModuleActiveRadiator]]
+			{
+				@DATA
+				{
+					@maxEnergyTransfer = 72.91625
+					@RESOURCE[ElectricCharge]
+					{
+						@rate = 0.064375
+					}
+				}
+			}
+		}
+	}
+}
+
+
+//	ITS Z1
+//	Diameter:	4.2m (13.8ft)
+//	Length:		4.9m (16ft)
+//	Mass:		8,755kg (19,300lb)
+//	Source:		http://spacecraftearth.com/#smoothscroll-portfolio-module
+//	Source:		https://space.skyrocket.de/doc_sdat/its-z1.htm
+@PART[ht2_truss_Z1_v2]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Z1 Truss Segment
+	@manufacturer = #roMfrBoeing
+	@description = The first truss piece, the Z1 truss, launched aboard STS-92 in October 2000. It contains the control moment gyroscope (CMG) assemblies, electrical wiring, communications equipment, and two plasma contactors designed to neutralize the static electrical charge of the space station. Another objective of the Z1 truss was to serve as a temporary mounting position for the "P6 truss and solar array" until its relocation to the end of the P5 truss during STS-120. Though not a part of the main truss, the Z1 truss was the first permanent lattice-work structure for the ISS, very much like a girder, setting the stage for the future addition of the stations major trusses or backbones.
+	@mass = 8.755
+	@specLevel = operational
+	%skinTempTag = Steel
+	%internalTempTag = Instruments
+	@RESOURCE[ElectricCharge]
+	{
+		@amount = 1000
+		@maxAmount = 1000
+	}
+	%reactionWheelPowerDraw = 2
+	%reactionWheelMode = CMG
+}
+
+
+//	Truss Port
+@PART[ht2_trussPort]:HAS[#category[Coupling]]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Truss Connector
+	@manufacturer = #roMfrBoeing
+	@description = Small Docking Port for the ISS Truss Structure.
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Truss Port Circle
+@PART[ht2_TTS_circle]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Truss Connector (Type C)
+	@manufacturer = #roMfrBoeing
+	@description = Small Docking Port for the ISS Truss Structure.
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Truss Port Compact
+@PART[ht2_TTS_compact]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Truss Connector (Compact)
+	@manufacturer = #roMfrBoeing
+	@description = Small Docking Port for the ISS Truss Structure.
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Truss Port Hex
+@PART[ht2_TTS_hex]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Truss Connector (Type B)
+	@manufacturer = #roMfrBoeing
+	@description = Small Docking Port for the ISS Truss Structure.
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Truss Port Semi Hex
+@PART[ht2_TTS_semiHex]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Truss Connector (Type A)
+	@manufacturer = #roMfrBoeing
+	@description = Small Docking Port for the ISS Truss Structure.
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Truss Port Mounted Angle
+@PART[ht2_TTS_standoff_angle]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Truss Connector (Mounted Angle)
+	@manufacturer = #roMfrBoeing
+	@description = Small Docking Port for the ISS Truss Structure.
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Truss Port Mounted
+@PART[ht2_TTS_standoff]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = ISS Truss Connector (Mounted)
+	@manufacturer = #roMfrBoeing
+	@description = Small Docking Port for the ISS Truss Structure.
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
\ No newline at end of file
diff --git a/GameData/RealismOverhaul/RO_SuggestedMods/HabTech2/RO_HabTechRobotics.cfg b/GameData/RealismOverhaul/RO_SuggestedMods/HabTech2/RO_HabTechRobotics.cfg
new file mode 100644
index 0000000000..0c794e6139
--- /dev/null
+++ b/GameData/RealismOverhaul/RO_SuggestedMods/HabTech2/RO_HabTechRobotics.cfg
@@ -0,0 +1,226 @@
+//	================================================================================
+//	HabTechRobotics
+//	================================================================================
+
+
+//	Canadarm 1 Mass: 410kg
+//	Canadarm 2 Mass: 1497kg
+//	JEM-RMS Mass: 780kg
+
+//	Note: Individual Part Masses are not known, everything will add up to the final sourced masses.
+
+//	Sources:
+//	https://www.asc-csa.gc.ca/eng/iss/canadarm2/canadarm-canadarm2-canadarm3-comparative-table.asp
+//	https://www.eoportal.org/satellite-missions/iss-jem
+
+
+//	================================================================================
+//	Canadarm 2
+//	================================================================================
+
+
+//	Boom 2
+@PART[ht_canadarm2_boom]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Canadarm 2 Structural Boom Unit
+	@manufacturer = Canadian Space Agency (CSA)
+	@mass = 0.15 // 4 per arm
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Latching End Effector 2
+@PART[ht_canadarm2_LEE]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Canadarm 2 Latching End Effector
+	@manufacturer = Canadian Space Agency (CSA)
+	@mass = 0.1485 // 2 per arm
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Servo 2
+@PART[ht_canadarm2_servo]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Canadarm 2 Servo Joint
+	@manufacturer = Canadian Space Agency (CSA)
+	@mass = 0.075 // 8 per arm
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	================================================================================
+//	JEM Robotic Manipulator System
+//	================================================================================
+
+
+//	RMS Boom
+@PART[ht_JEM_RMS_boom]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = JEM RMS Structural Boom Unit
+	@manufacturer = #roMfrMHI
+	@mass = 0.13 // 2 per arm
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	RMS Servo
+@PART[ht_JEM_RMS_servo]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = JEM RMS Servo Joint
+	@manufacturer = #roMfrMHI
+	@mass = 0.06 // 7 per arm
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	================================================================================
+//	Canadarm 1
+//	================================================================================
+
+
+//	Boom 1
+@PART[ht_C1_boom]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Canadarm 1 Structural Boom Unit
+	@manufacturer = Canadian Space Agency (CSA)
+	@mass = 0.09 // 2 per arm
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Elbow 1
+@PART[ht_C1_elbow]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Canadarm 1 Elbow Servo Joint
+	@manufacturer = Canadian Space Agency (CSA)
+	@mass = 0.04 // 2 per arm
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Latching End Effector 1
+@PART[ht_C1_LEE]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Canadarm 1 Latching End Effector
+	@manufacturer = Canadian Space Agency (CSA)
+	@mass = 0.1 // 1 per arm
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Pitch Joint 1
+@PART[ht_C1_pitch]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Canadarm 1 Servo Pitch Joint
+	@manufacturer = Canadian Space Agency (CSA)
+	@mass = 0.04 // 2 per arm
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	Rotator 1
+@PART[ht_C1_rotator]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Canadarm 1 Axial Servo Joint
+	@manufacturer = Canadian Space Agency (CSA)
+	@mass = 0.02 // 2 per arm
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	================================================================================
+//	Attachment Points
+//	================================================================================
+
+
+//	Grapple Fixture
+@PART[ht_grappleFixture]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Canadarm FGRS Grapple Fixture
+	@manufacturer = Canadian Space Agency (CSA)
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	JEM RMS Grapple Fixture
+@PART[ht_grappleFixtureKibo]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = JEM RMS EMGF Experiment Grapple Fixture
+	@manufacturer = #roMfrMHI
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
+
+
+//	PDGF
+@PART[ht_PDGF]:FOR[RealismOverhaul]
+{
+	%RSSROConfig = True
+	!rescaleFactor,* = DEL
+	%rescaleFactor = 1.8
+	@title = Canadarm PDGF Power-Data Grapple Fixture
+	@manufacturer = Canadian Space Agency (CSA)
+	@specLevel = operational
+	%skinTempTag = Aluminum
+	%internalTempTag = Instruments
+}
\ No newline at end of file
diff --git a/GameData/RealismOverhaul/Waterfall_Configs/Benjee10_Mods/Benjee10_HabTech2.cfg b/GameData/RealismOverhaul/Waterfall_Configs/Benjee10_Mods/Benjee10_HabTech2.cfg
new file mode 100644
index 0000000000..ad8ba7f4fb
--- /dev/null
+++ b/GameData/RealismOverhaul/Waterfall_Configs/Benjee10_Mods/Benjee10_HabTech2.cfg
@@ -0,0 +1,43 @@
+//	================================================================================
+//	Benjee10 HabTech 2 Waterfall
+//	================================================================================
+
+
+// Camera Mast
+@PART[ht2_cameraMast]:BEFORE[ROWaterfall]:NEEDS[Waterfall]
+{
+	@MODULE[ModuleWaterfallFX]
+	{
+		@TEMPLATE
+		{
+			@scale = 1.81, 1.81, 1.81
+		}
+	}
+}
+
+
+// Prop Module
+@PART[ht2_SCRAM]:BEFORE[ROWaterfall]:NEEDS[Waterfall]
+{
+	@MODULE[ModuleWaterfallFX]
+	{
+		@TEMPLATE
+		{
+			@scale = 1.629, 1.7195, 1.629
+		}
+	}
+}
+
+
+//	RCS and Prop Module
+@PART[ht2_propModule|ht2_rcs_*]:BEFORE[ROWaterfall]:NEEDS[Waterfall]
+{
+	ROWaterfall
+	{
+		autoConfig = rcs
+		transform = rcs
+		position = 0,0,0
+		rotation = 180, 0, 0
+		scale = 0.85, 0.85, 0.85
+	}
+}
\ No newline at end of file