Shuttle mission requirements and cost objectives have led to the selection of a Shuttle-Attached Manipulator System (SAMS) as a general purpose mechanism for docking, payload handling, and the general launch and retrieval of free-flying satellites. SAMS design requirements are discussed, giving attention to end effectors, kinematics, timelines, dynamics, load ratings, TV cameras and lights. Requirements for low-cost payload satellites are considered, taking into account satellites with modular subsystems which are designed for replacement and for resupply in orbit by SAMS.
Shuttle-Attached Manipulator System requirements.
National Conference on Remotely manned systems: Exploration and operation in space ; 1972 ; Pasadena, CA
1973-01-01
Miscellaneous
No indication
English
Shuttle remote manipulator collision-avoidance system
Tema Archive | 1985
|Shuttle remote manipulator system hardware test facility
NTRS | 1980
|Development of a shuttle manipulator simulator
Tema Archive | 1976
|