The expanded scientific capabilities available by interfacing an orbital, free-flying experiments platform with Shuttle tending are outlined. The platform would be lifted to orbit by the Shuttle, and modularly increased in size on subsequent flights. Science packages could be left on the 26,000 lb space platform for up to six months. Component sections would include electrical and thermal control systems, berthing ports for payloads and an Orbiter, and an attitude control, communications, and data handling subsection. A 12 kW solar array would furnish power, and interconnect with Spacelab would further enhance the operations range. All berthed science packages would have individual pointing ability and grapples for the Orbiter RMS. Eventual evolution to include facilities for a human crew and a 25 kW solar array is projected.
Space platforms
1983-04-01
Miscellaneous
No indication
English
NTRS | 1981
|NTRS | 1986
|Space platforms / MBB Raumfahrt ; Vol. 2: LEO platforms
TIBKAT | 1982
|Morphing Tensegrity Space Platforms
AIAA | 2021
|Online Contents | 1994
|