| 发明名称 |
SPACECRAFT WITH OPEN SIDES |
| 摘要 |
A spacecraft may include a module structure having a plurality of module sides. The spacecraft may include a central cylinder extending through a center of the spacecraft. The central cylinder may be the only closed cross-section extending along a longitudinal axis of the spacecraft. |
| 申请公布号 |
US2014239124(A1) |
申请公布日期 |
2014.08.28 |
| 申请号 |
US201313781483 |
申请日期 |
2013.02.28 |
| 申请人 |
The Boeing Company |
发明人 |
ASTON Richard W.;TOMZYNSKA Anna M. |
| 分类号 |
B64G1/40;B64G1/54;B64G1/44 |
主分类号 |
B64G1/40 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A spacecraft, comprising:
a module structure of a spacecraft having a plurality of module sides; a central cylinder extending through a center of the spacecraft; and the central cylinder being the only closed cross-section extending along a longitudinal axis of the spacecraft. |
| 地址 |
US |
