This standard defines the requirements and characteristics of electrical power for spacecraft. This standard also defines analysis, verification, and testing methodologies to be used to ensure that the loads operate when connected to the specified power quality and performance as defined by this standard.
| Author |
SAE
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| Editor |
SAE
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| Document type |
Standard
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| Format |
File
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| ICS |
49.140 : Space systems and operations
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| Number of pages |
34
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| Replace |
SAE AS 5698:2012-04-11
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| Set |
AEROPAKS10U-10
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| Year |
2018
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| Document history |
SAE AS 5698:2012-04-11
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| Country |
USA
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| Keyword |
SAE 5698;SAE AS5698A;SAE AS5698A;SAE AS 5698
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