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Results of tests of insta-foam thermal protection system (tps) material for protection of equipment inside the srb aft skirt
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Dean, W. G. |
| Copyright Year | 1982 |
| Description | The objective of these tests was to determine whether Insta-Foam can be used successfully to protect items inside the solid rocket booster aft skirt during reentry. On some of the early Space Shuttle flights the aft skirt heat shield curtain failed during reentry. This allowed the hot gases to damage some of the equipment, etc., inside the skirt. For example, some of the propellant lines were overheated and ruptured and some of the NSI (nozzle severance) cables were damaged. It was suggested that the Insta-Foam thermal protection system be sprayed over these lines, etc., to protect them during future flights in case of a curtain failure. The tests presented were devised and run to check out the feasibility of this idea. |
| File Size | 1213607 |
| Page Count | 16 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850026982 |
| Archival Resource Key | ark:/13960/t29932c9g |
| Language | English |
| Publisher Date | 1982-08-03 |
| Access Restriction | Open |
| Subject Keyword | Nonmetallic Materials Foams Manned Reentry Reentry Effects Thermal Protection Calibrating Space Shuttles Solid Propellant Rocket Engines Heat Shielding Feasibility Analysis Models 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 |
