The Mini Pressurized Logistic Module (MPLM) is designed to transport cargo inside the Space Station Freedom. Results obtained from a preliminary design of the heat rejection and temperature control system are reported. Particular evidence is given to the combined cabin/avionics air loop design. This solution allows significant advantages to be gained in terms of mass, cost, control simplification, with respect to the more traditional approach which foresees separated cabin and avionics air loops.
Combined Cabin/Avionics Air Loop Design for the Space Station Logistic Module
1991
5 pages
Report
Keine Angabe
Englisch
Manned Spacecraft , Life Support Systems , Air purification , Avionics , Pressurized cabins , Spacecraft cabin atmospheres , Temperature control , Columbus space station , Cooling systems , Environmental control , Heat radiators , Spacecraft design , Spacecraft temperature , Systems engineering , Foreign technology
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