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1.1 Purpose:
1.1.1 The primary purpose of this practice is to provide guidance for making adequate thermal balance tests of spacecraft and components where solar simulation has been determined to be the applicable method. Careful adherence to this practice should ensure the adequate simulation of the radiation environment of space for thermal tests of space vehicles.
| Author | ASTM |
|---|---|
| Editor | ASTM |
| Document type | Standard |
| Format | File |
| Confirmation date | 2015-10-01 |
| ICS | 49.140 : Space systems and operations |
| Number of pages | 34 |
| Replace | ASTM E491-73(2010) |
| Set | ASTMVOL1503 |
| Year | 2004 |
| Document history | |
| Country | USA |
| Keyword | ASTM 491;ASTM E491;ASTM E491;10.1520/E0491-73R15 |