Results of design analysis and selection of configuration and subsystems to perform rendezvous; propellant storage is of prime consideration and 5 basic tank and structural support designs are incorporated and compared; provisions made for following subsystems; guidance and attitude control, propulsion system, radar, power supply, environmental control, mission payloads, data storage, and telemetry and command equipment.
Space vehicle design for unmanned rendezvous
Astronautical Sciences Rev
Astronautical Sciences Review ; 3 , n 4
1961
9 pages
Article (Journal)
English
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