A simultaneous spin/eject mechanism was developed for aerospace applications requiring a compact, passive device which would accommodate payload support and controlled-release functions, and which would provide a highly accurate spin-ejection motion to the payload. The mechanism satisfied the requirements and is adaptable to other deployment applications.
A simultaneous spin/eject mechanism for aerospace payloads
01.07.1976
Aufsatz (Konferenz)
Keine Angabe
Englisch
SLUB | 1989
SLUB | 1989
British Library Online Contents | 1996
|British Library Conference Proceedings | 1996
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