发明名称 |
Payload deployment from shuttle with linear and angular velocity |
摘要 |
A payload such as a spacecraft is deployed from launch vehicle with linear and angular velocity, using a structural arrangement for applying a tangential, single point ejection force to the spacecraft, in which, the single point ejection force and the spacecraft/launch vehicle reaction points enclose the spacecraft center of mass and center of percussion.
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申请公布号 |
US4359201(A) |
申请公布日期 |
1982.11.16 |
申请号 |
US19800125807 |
申请日期 |
1980.02.28 |
申请人 |
HUGHES AIRCRAFT COMPANY |
发明人 |
THOMSON, GRAHAM S.;WITTMANN, ALOIS |
分类号 |
B64G1/22;B64G1/64;(IPC1-7):B64G1/64 |
主分类号 |
B64G1/22 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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