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SAE AIR 1168/11A:2011-07-25
Spacecraft Boost and Entry Heat Transfer (Stabilized: Jul 2011)More info
The prediction of vehicle temperatures during ascent through the earth’s atmosphere requires an accurate knowledge of the aerodynamic heating rates occurring at the vehicle surface. Flight parameters required in heating calculations include the local airstream velocity, pressure, and temperature at the boundary layer edge for the vehicle location in question. In addition, thermodynamic and transport air properties are required at these conditions.
| Author | SAE |
|---|---|
| Editor | SAE |
| Document type | Standard |
| Format | File |
| ICS | 49.140 : Space systems and operations |
| Number of pages | 290 |
| Replace | SAE AIR 1168/11:2008-02-19 |
| Set | AEROPAKS10U-10 |
| Year | 2011 |
| Document history | SAE AIR 1168/11:2008-02-19 |
| Country | USA |
| Keyword | SAE 116811;SAE AIR1168/11A;SAE AIR1168/11A;SAE AIR 1168/11 |