发明名称 |
FUNCTIONALLY AND STRUCTURALLY MODULAR PARALLELOGRAM-SHAPED SPACECRAFT |
摘要 |
A functionally and structurally modular, parallelogram-shaped spacecraft (102). The spacecraft (102) includes a plurality of modules joined to one another along an axis of the spacecraft, wherein each module is devoted to a particular function of the spacecraft, and wherein all of the modules have the same cross-sectional size and geometry. The geometry is approximately a parallelogram in a plane normal to the axis of the spacecraft. The functions include power, processing, propulsion, and the like.
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申请公布号 |
WO0051887(A9) |
申请公布日期 |
2001.08.30 |
申请号 |
WO2000US05754 |
申请日期 |
2000.03.06 |
申请人 |
LOCKHEED MARTIN MISSILES AND SPACE |
发明人 |
ANDERSON, THOMAS, W.;BAY, F., M.;BONHAM, JOHN |
分类号 |
B64G1/00;B64G1/10;(IPC1-7):B64G1/22 |
主分类号 |
B64G1/00 |
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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