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卫星用复合材料气瓶性能

张建宝 林松 王俊锋 孙宏杰 蒋文革

宇航材料工艺2013,Vol.43Issue(4):67-69,3.
宇航材料工艺2013,Vol.43Issue(4):67-69,3.

卫星用复合材料气瓶性能

Performance of Composite Overwrapped Pressure Vessel Applied on Secondary Planet

张建宝 1林松 1王俊锋 1孙宏杰 1蒋文革1

作者信息

  • 1. 航天材料及工艺研究所,北京100076
  • 折叠

摘要

Abstract

The experiments are studied in epoxy resin cast mechanical property,NOL hoop mechanical property,surface property of metallic inner wall,vacuum outgassing of composite and composite pressure vessel,aimed to the manufacturing of composite overwrapped pressure vessels(COPV) on the propulsion system of satellites.The result shows that the burst pressure of the COPV is 86 MPa after 150 times fatigue experiments,the vessel characteristic factor is 57.7 km,and the COPV is suitable for the application needing in vacuum.

关键词

纤维缠绕/复合材料气瓶/爆破压强/碳纤维

Key words

Filament wound/ Composite pressure vessel/ Burst pressure/ Carbon fiber

引用本文复制引用

张建宝,林松,王俊锋,孙宏杰,蒋文革..卫星用复合材料气瓶性能[J].宇航材料工艺,2013,43(4):67-69,3.

宇航材料工艺

OA北大核心CSCDCSTPCD

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