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.
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
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