Changes to Russia’s Contribution to the ISS Under Evaluation
Note: The following is an excerpt from CR 6291 USOS Core Complete Development Guidelines/Questions, 19 December 2001 [SSCB Baseline of Assembly Sequence Rev. C], (Powerpoint), NASA MSFC
Russian Configuration Changes
– the DC1 is relocated from the SM nadir to the SM zenith using the SSRMS
– There is no pressurized compartment or centralized heat rejection system
Delivered on 2 carriers and assembled on-orbit (The first carrier is installed on the relocated DC1 using the SSRMS)
-The ERA is used for the final deployment of SPP
– Articulating solar arrays and a deployed radiator
– Provides distribution of SPP power to the Russian Segment
– Only 2 mechanisms provided for the Research Modules
Background
– For example, there are 3 SPP concepts still under consideration
Isometric View from Starboard Side
Zenith View
VERY Preliminary Russian Segment EVA Plan
Details of EVA, flight, and configuration interdependencies are preliminary
— These are estimates based on concepts and will change
Deferred EVAs
Solar Array augmentation – 4 EVAs (may or may not happen)
DC1 relocation – 4 EVAs
MPM – 3 EVAs
SPP-U installation – 5 EVAs
UDM – 4 EVAs
SPP-U – 4 EVAs
RM1 – 4 EVAs
RM2 – 4 EVAs
Additional EVAs may be required during Shuttle flights