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Wind tunnel tests of space shuttle solid rocket booster insulation material in the aerothermal tunnel c
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Nutt, K. W. Hartman, A. S. |
| Copyright Year | 1982 |
| Description | Wind tunnel tests of the space shuttle Solid Rocket Booster Insulation were conducted in the von Karman Gas Dynamics Facility Tunnel C. For these tests, Tunnel C was run at Mach 4 with a total temperature of 1100-1440 and a total pressure of 100 psia. Cold wall heating rates were changed by varying the test article support wedge angle. Selected results are presented to illustrate the test techniques and typical data obtained. |
| File Size | 2813899 |
| Page Count | 55 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19830011537 |
| Archival Resource Key | ark:/13960/t6qz72g9q |
| Language | English |
| Publisher Date | 1982-11-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Space Shuttles Aerodynamic Heating Thermal Insulation Wind Tunnel Tests Solid Propellant Rocket Engines External Stores Heat Transfer 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 |
