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For small spacecraft cone - rod flexible wall docking mechanism design studies

Author: HanWei
Tutor: HuangZuoYong
School: National University of Defense Science and Technology
Course: Aeronautical and Astronautical Science and Technology
Keywords: Autonomous on-orbit service Spacecraft Docking mechanism Contact-impact ANSYS / LS-DYNA Damper system
CLC: V526
Type: Master's thesis
Year: 2011
Downloads: 32
Quote: 0
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Abstract


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CLC: > Aviation, aerospace > Aerospace ( Astronauts ) > Aerospace surgery > Docking technology
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