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Srb environment evaluation and analysis. volume 1: redesigned srb flight heating evaluation
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Crain, William K. |
| Copyright Year | 1991 |
| Description | Following the Space Shuttle STS-51L disaster on January 28, 1986, a considerable redesign effort was launched on the Solid Rocket Booster. This effort culminated in three instrumented flights, STS-26R, 27R, and 29R, beginning in September of 1989. Aeroheating data were obtained on these flights in the form of pressure, heat flux, and gas temperature probe measurements. These data were analyzed from an ascent and reentry heating point of view. The flight data were verified, compared with historic and theoretical results, and scaled to design. Impact of these results on the current design environment set was assessed and recommendations made. This report documents this effort. |
| File Size | 16326089 |
| Page Count | 400 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930016864 |
| Archival Resource Key | ark:/13960/t8jd9s86h |
| Language | English |
| Publisher Date | 1991-09-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Flight Tests Reentry Trajectories Flight Instruments Gas Temperature Design Analysis Space Shuttle Boosters Plumes Heat Flux Reentry Effects Ascent Aerodynamic Heating Skirts Thermal Analysis Frustums 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 |
