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Study of solid rocket motors for a space shuttle booster. appendix c: recovery and reuse 120-inch diameter solid rocket motor boosters
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1972 |
| Description | A baseline for a space shuttle configuration utilizing four parallel-burn 120-in. diameter SRMS is presented. Topics discussed include parachute system sequence, recovery system development profile, parachute container, and segment and closure recovery operations. A cost analysis for recovery of the SRM stage is presented. It is concluded that from the standpoint of minimum cost and development, parachutes are the best means of achieving SRM recovery. Major SRM components can be reused safely. |
| File Size | 1776881 |
| Page Count | 43 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720015138 |
| Archival Resource Key | ark:/13960/t6tx8396d |
| Language | English |
| Publisher Date | 1972-03-15 |
| Access Restriction | Open |
| Subject Keyword | Propulsion Systems Recovery Parachutes Systems Engineering Solid Propellant Rocket Engines Booster Recovery Cost Analysis Space Shuttle Boosters Research and Development Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |