SPACE_DEBRIS

作品数:72被引量:138H指数:6
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相关期刊:《Journal of Beijing Institute of Technology》《Frontiers of Information Technology & Electronic Engineering》《Science China(Physics,Mechanics & Astronomy)》《Aerospace China》更多>>
相关基金:国家自然科学基金国家高技术研究发展计划中国博士后科学基金更多>>
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Cutting-Edge Space Exploration Technology Maturity Level Facilitation with Support of Space Debris Removal Missions被引量:2
《Journal of Beijing Institute of Technology》2018年第4期477-484,共8页Hamed Ahmadloo Jingrui Zhang 
Supported by the National Natural Science Foundation of China(11572037)
Considering current space debris situation in outer space environment,different methods for debris removal missions are proposed.In addition,advanced technologies are needed to be demonstrated for future human space e...
关键词:space debris removal missions technology demonstrator missions technology readiness level drag augmentation methods 
Simple Method for Tethered Space Debris Retrieval
《Journal of Beijing Institute of Technology》2017年第1期5-8,共4页Bensong Yu Dongping Jin 
Supported by the Natural Science Foundation of China(11672125);the Fundamental Research Funds for the Central Universities(NS2016009)
Space debris retrieval problem utilizing a tethered system in an elliptical orbit is studied in this paper.An analytical control law specified by a tether length rate for retrieval is derived from a dumbbell model of ...
关键词:space debris RETRIEVAL analytical control law STABILITY 
Experimental Study of Hypervelocity Impact on Multi-Shock Structure被引量:1
《Journal of Beijing Institute of Technology》2004年第3期274-279,共6页张庆明 陈沿海 黄风雷 
SponsoredbytheNational863ProgramProject ( 2 0 0 3AA7410 2 1)
Hypervelocity impact tests on multi-shock shields are carried out in order to develop space structures (against) space debris impacts. Sheets of LY12 aluminum were used as bumpers. The total thickness of shield struct...
关键词:HYPERVELOCITY multi-sheet structure debris cloud space debris 
Experimental Study and Numerical Simulation of Hypervelocity Projectile Impact on Double-Wall Structure被引量:1
《Journal of Beijing Institute of Technology》2004年第3期280-284,共5页陈沿海 张庆明 黄风雷 
SponsoredbytheNational863ProgramProject( 2 0 0 3AA7410 2 1)
Tests of hypervelocity projectile impact on double-wall structure were performed with the front wall ranging from 0.5 mm to 2.0 mm thick and different impact velocities. Smooth particle hydrodynamics (SPH) code in LS-...
关键词:hypervelocity impact double-wall structure SPH space debris spacecraft shield 
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