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SAE AIR 1168/13A:2011-07-25
Spacecraft Equipment Environmental Control (Stabilized: Jul 2011)More info
This part of the manual presents methods for arriving at a solution to the problem of spacecraft inflight equipment environmental control. The temperature aspect of this problem may be defined as the maintenance of a proper balance and integration of the following thermal loads: equipment-generated, personnel-generated, and transmission through external boundary.
| Author | SAE |
|---|---|
| Editor | SAE |
| Document type | Standard |
| Format | File |
| ICS | 49.140 : Space systems and operations |
| Number of pages | 172 |
| Replace | SAE AIR 1168/13:2006-03-24 |
| Set | AEROPAKS10U-10 |
| Year | 2011 |
| Document history | SAE AIR 1168/13:2006-03-24 |
| Country | USA |
| Keyword | SAE 116813;SAE AIR1168/13A;SAE AIR1168/13A;SAE AIR 1168/13 |