A 60 kW solar power array was designed. It features a multiple deployment/retraction capability and a multiple stowage/restowage capability. It allows for power growth and can provide a wide voltage range. Blanket construction is modular. It is compatible with orbiters, power module-type vehicles and the free flying pallet. It has remote manipulator system and extravehicular activity interfaces.
Sola: Solar Array Technology Development for Shuttle Launched Missions
1981
110 pages
Report
Keine Angabe
Englisch
Design and technology of solar arrays for shuttle launched missions
Tema Archiv | 1980
|AIAA | 2001
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