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A simultaneous spin/eject mechanism for aerospace payloads
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Palmer, G. D. Banks, T. N. |
| Copyright Year | 1976 |
| Description | 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. |
| File Size | 487101 |
| Page Count | 10 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760021200 |
| Archival Resource Key | ark:/13960/t01z9047b |
| Language | English |
| Publisher Date | 1976-07-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Equipment Specifications Spacecraft Components Releasing Spin Ejection Payloads Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
