ZHAI Shao-xiong, WANG Zhang-sheng, ZHANG Wei-wen, et al. DEVELOPMENT OF THE SOLAR WING HINGE MODULE TEST SYSTEM APPLIED IN THERMAL VACUUM ENVIRONFEMT[J]. VACUUM AND CRYOGENICS, 2004, 10(4): 202-204.
Citation:
ZHAI Shao-xiong, WANG Zhang-sheng, ZHANG Wei-wen, et al. DEVELOPMENT OF THE SOLAR WING HINGE MODULE TEST SYSTEM APPLIED IN THERMAL VACUUM ENVIRONFEMT[J]. VACUUM AND CRYOGENICS, 2004, 10(4): 202-204.
ZHAI Shao-xiong, WANG Zhang-sheng, ZHANG Wei-wen, et al. DEVELOPMENT OF THE SOLAR WING HINGE MODULE TEST SYSTEM APPLIED IN THERMAL VACUUM ENVIRONFEMT[J]. VACUUM AND CRYOGENICS, 2004, 10(4): 202-204.
Citation:
ZHAI Shao-xiong, WANG Zhang-sheng, ZHANG Wei-wen, et al. DEVELOPMENT OF THE SOLAR WING HINGE MODULE TEST SYSTEM APPLIED IN THERMAL VACUUM ENVIRONFEMT[J]. VACUUM AND CRYOGENICS, 2004, 10(4): 202-204.
DEVELOPMENT OF THE SOLAR WING HINGE MODULE TEST SYSTEM APPLIED IN THERMAL VACUUM ENVIRONFEMT
A test system used in the test of key mechanical parameters of the solar wing hinge module under thermal vacuum environment was developed. The components of the test system were introduced in detail and the important units were designed concretely. The test results acquired by the system are accurate and credible. The good effects are achieved in application fields.
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