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| Space Vehicle Test Baseline and Level Adjustment of US Military Standard |
| Received:March 21, 2020 Revised:April 15, 2020 |
| View Full Text View/Add Comment Download reader |
| DOI：10.7643/issn.1672-9242.2020.05.014 |
| KeyWord:US military standard space vehicle test MIL-STD-1540 SMC-S-016 baseline test level tailor |
| Author | Institution |
| LI Xi-yuan |
Beijing Institute of Spacecraft Environment Engineering, Beijing , China;Beihang University, Beijing , China |
| JIA Rui-jin |
Beijing Institute of Spacecraft Environment Engineering, Beijing , China |
| SUN Xue-yin |
Beijing Institute of Spacecraft Environment Engineering, Beijing , China |
| SHANG Yong-hong |
Beijing Institute of Spacecraft Environment Engineering, Beijing , China |
| SUN Yu-wei |
Beijing Institute of Spacecraft Environment Engineering, Beijing , China |
| PEI Yi-fei |
Beijing Institute of Spacecraft Environment Engineering, Beijing , China |
| WANG Jing |
Beijing Institute of Spacecraft Environment Engineering, Beijing , China |
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| Abstract: |
| The development of military standards for spacecraft test in the United States was investigated. The development of MIL-STD-154 standard to SMC-S-016A standard was systematically sorted out. The revision of system level and component level test baseline was sorted out and analyzed. Taking the thermal test as a typical research object, the modification of different standards for the system level and component level thermal test in the test temperature range, cycle number and tailoring method were sorted out, the changes of test baseline and test level were compared, and the basis for revision was analyzed in combination with the development of spacecraft model and verification concept in the United States. It provides a reference for the formulation and revision of corresponding standards in China. |
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