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つくばリポジトリ AERJ 121 1241 970

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Fig. 2:  ETS-VIII lau nched in 2006  (©JAXA)Satellite body
Figure 5 shows an overview of one module. The LDR consists of CFRP tubes and titanium alloy joints
Fig. 7:  Modelling of an automatic open umbrella mechanism Spring force
Fig. 8: Applied thermal history Time [min]Temperature [℃]0 100 200 300 400 500-150-100-50050TATB
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