NASA NTRS · 19760021200
A simultaneous spin/eject mechanism for aerospace payloads
Abstract
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.
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Palmer, G. D., Banks, T. N.. 1976-07-01. A simultaneous spin/eject mechanism for aerospace payloads. https://ntrs.nasa.gov/citations/19760021200
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