发明名称 |
METHOD AND APPARATUS FOR SATELLITE ORBITAL CHANGE USING SPACE DEBRIS |
摘要 |
An apparatus for orbital change of a satellite incorporates a capture mechanism for space debris and a tether connecting the capture mechanism to a satellite. The tether is extendable to position the capture mechanism relative to the space debris. A controller is employed for timed release of the space debris by the capture mechanism for orbital change by the satellite.
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申请公布号 |
US2010193640(A1) |
申请公布日期 |
2010.08.05 |
申请号 |
US20090362902 |
申请日期 |
2009.01.30 |
申请人 |
THE BOEING COMPANY |
发明人 |
ATMUR ROBERT J.;PENZO, II LEONARD A. |
分类号 |
B64G1/66;B64G1/10;B64G1/22 |
主分类号 |
B64G1/66 |
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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