发明名称 |
Modular core structure for dual-manifest spacecraft launch |
摘要 |
<p>A spacecraft may include an upper core structure (148) or a lower core structure (168). The upper core structure (148) may include an upper cylinder (150) for supporting an upper spacecraft (146) of a dual-manifest launch configuration. The lower core structure (168) may include a lower cylinder (170) for supporting a lower spacecraft (166) with the upper cylinder (150) mounted on top of the lower cylinder (170). The upper cylinder (150) may have an upper cylinder inner diameter that may be substantially similar to the lower cylinder inner diameter.</p> |
申请公布号 |
EP2772441(A2) |
申请公布日期 |
2014.09.03 |
申请号 |
EP20140156420 |
申请日期 |
2014.02.24 |
申请人 |
THE BOEING COMPANY |
发明人 |
ASTON, RICHARD;TOMZYNSKA, ANNA;LANGMACK, MICHAEL;PETERKA, JAMES |
分类号 |
B64G1/00;B64G1/10 |
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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