| 发明名称 |
SPACE SHUTTLE ORBITER AND RETURN SYSTEM |
| 摘要 |
A launch system comprises a nose section comprising a nose coupling surface, a tail section comprising a tail coupling surface facing the nose coupling surface and a mast coupling the nose and tail sections. The mast is configured to expand and retract to displace the nose and tail sections within a range of distances from one another. In a retracted state, the nose and tail sections are either structurally coupled to one another at the nose and tail coupling surfaces or structurally coupled to at least one integrated module located between the nose and the tail sections. |
| 申请公布号 |
US2014319281(A1) |
申请公布日期 |
2014.10.30 |
| 申请号 |
US201313870916 |
申请日期 |
2013.04.25 |
| 申请人 |
Helou, JR. Elie |
发明人 |
Helou, JR. Elie |
| 分类号 |
B64G1/14;B64G1/40;B64G1/58;B64G1/00;B64G1/22 |
主分类号 |
B64G1/14 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A launch system comprising:
a nose section comprising a nose coupling surface; a tail section comprising a tail coupling surface facing the nose coupling surface; and a mast coupling the nose and tail sections, the mast being configured to expand and retract to displace the nose and tail sections within a range of distances from one another; wherein in a retracted state, the nose and tail sections are either structurally coupled to one another at the nose and tail coupling surfaces or structurally coupled to at least one integrated module located between the nose and the tail sections. |
| 地址 |
Santa Barbara CA US |
