Loading...
Please wait, while we are loading the content...
Similar Documents
Shuttle srb preflight/post-flight thermal assessment
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1985 |
| Description | The development of the thermal protection system for the Solid Rocket Booster is reported. Tests and analytical efforts were conducted and new problems are continually attacked and solved. During the first six Shuttle flights it was necessary to make a final thermal assessment of the TPS and structural systems temperatures. The thermal assessments were made and are compared with post flight data. |
| File Size | 797997 |
| Page Count | 9 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19860011023 |
| Archival Resource Key | ark:/13960/t4sj6c36m |
| Language | English |
| Publisher Date | 1985-12-05 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Flight Tests Performance Tests Thermal Protection Aerodynamic Heating Space Shuttle Missions Heat Shielding Thermal Analysis Space Transportation System Booster Rocket Engines Space Shuttle Boosters Aerothermodynamics 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 |
