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Space shuttle program solid rocket booster decelerator subsystem
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Barnard, J. W. |
| Copyright Year | 1985 |
| Description | The recovery of the Solid Rocket Boosters presented a major challenge. The SRB represents the largest payload ever recovered and presents the added complication that it is continually emitting hot gases and burning particles of insulation and other debris. Some items, such as portions of the nozzle, are large enough to burn through the nylon parachute material. The SRB Decelerator Subsystem program was highly successful in that no SRB has been lost as a result of inadequate performance of the DSS. |
| File Size | 7860408 |
| Page Count | 89 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19860006776 |
| Archival Resource Key | ark:/13960/t77t2kf2r |
| Language | English |
| Publisher Date | 1985-09-01 |
| Access Restriction | Open |
| Subject Keyword | Space Transportation Recovery Parachutes Parachute Fabrics Parachute Descent Space Shuttles Solid Propellant Rocket Engines Recoverable Launch Vehicles Booster Recovery Design Analysis Booster Rocket Engines Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
