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Spacecraft separation systems mechanisms: characteristics/performance during high altitude flight test from nasa wallops station, va.
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Pride, J. D. |
| Copyright Year | 1973 |
| Description | The applications of various separation mechanisms to meet flight mission goals within the physical and environmental constraints of a single stage rocket test vehicle are considered. Each separation concept was selected from the numerous choices available on the basis of its unique requirement and the flight test vehicle incorporated several different concepts. Attention to specific requirements and thoroughness in design and testing were essential to success since there is no specific single answer to separation problems. |
| File Size | 3283030 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740003569 |
| Archival Resource Key | ark:/13960/t9m37kt1t |
| Language | English |
| Publisher Date | 1973-10-01 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Stage Separation Performance Tests Systems Engineering High Altitude Tests Spacecraft Design Spacecraft Configurations Rocket Vehicles Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
