The Ku Band Subsystem for the Space Shuttle Orbiter must operate as rendezvous radar and provide two way communications with the ground. A discussion of accomplishing these objectives while meeting the additional requirements of minimum weight, limited stowage volume, and adequate cooling is presented.
KU band integrated radar/communications subsystem for the shuttle
Ein integriertes Radar- und Nachrichtensystem fuer die Raumfaehre (Space Shuttle) auf dem KU-Band
1977
6 Seiten, 13 Bilder, 6 Tabellen
Aufsatz (Konferenz)
Englisch
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