Paper demonstrates feasibility of assembling space rockets in orbit and of doing so with equipment and techniques already available; accuracy of satellite orbit discussed and arbitrary specification of orbit plane, apogee, and perogee vectors made; tracking and instrumentation problem and solutions discussed.
Problems associated with assembly of multiunit satellite in orbit
ASME -- Paper
ASME Meeting ; 1959
American Society of Mechanical Engineers -- Papers ; n 59-AV-25
1959
9 pages
Aufsatz (Konferenz)
Englisch
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