The International Space Station (ISS) Environmental Control and Life Support System (ECLSS) is continuing to evolve in the post-Space Shuttle era. The ISS vehicle configuration that is in operation was designed for docking of a Space Shuttle vehicle, and designs currently under development for commercial crew vehicles require different interfaces. The ECLSS Temperature and Humidity Control Subsystem (THC) Inter-Module Ventilation (IMV) must be modified in order to support two docking interfaces at the forward end of ISS, to provide the required air exchange. Development of a new higher-speed IMV fan and extensive ducting modifications are underway to support the new Commercial Crew Vehicle interfaces. This paper will review the new ECLSS IMV development requirements, component design and hardware status, subsystem analysis and testing performed to date, and implementation plan to support Commercial Crew Vehicle docking.
Inter-Module Ventilation Changes to the International Space Station Vehicle to Support Integration of the International Docking Adapter and Commercial Crew Vehicles
2015
10 pages
Report
Keine Angabe
Englisch
Life Support Systems , Unmanned Spacecraft , Manned Spacecraft , Space station modules , Ventilation , Ventilation fans , International space station , Spacecraft docking modules , Adapters , Spacecrews , Commercial spacecraft , Ducts , Air flow , Temperature , Humidity , Control systems design , Life support systems , Environmental control , Analysis (mathematics) , Computational fluid dynamics