发明名称 |
MODULAR SPACECRAFT SYSTEM |
摘要 |
TITLE OF THE INVENTION: MODULAR SPACECRAFT SYSTEM A modular spacecraft system adapted for orbital flight is capable of expansion by the connection of at least two substantially identical spacecraft modules, each of which is capable of independent operation. Each spacecraft module comprises a spacecraft body, at least one solar array extendible outwardly from the spacecraft body, and at least one structural interface means for connecting one spacecraft module to another spacecraft module. Methods for deployment of a spacecraft module and for assembly of a modular spacecraft system utilizing a reusable space vehicle are also disclosed. |
申请公布号 |
CA1282767(C) |
申请公布日期 |
1991.04.09 |
申请号 |
CA19860503215 |
申请日期 |
1986.03.04 |
申请人 |
SPACE INDUSTRIES, INC. |
发明人 |
FAGET, MAXIME A.;JOHNSON, CALDWELL C.;BERGERON, DAVID J., III |
分类号 |
B64G1/10;B64G1/00;B64G1/12;B64G1/14;B64G1/22;B64G1/34;B64G1/44;B64G1/64 |
主分类号 |
B64G1/10 |
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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