| 发明名称 |
TETHER FOR SPACECRAFT REACTION CONTROL SYSTEM |
| 摘要 |
A spacecraft reaction control system comprising: a spacecraft having a center of mass; a length of tether extending from said spacecraft and offset from said spacecraft's center of mass and means for controllably changing said extension of said offset such that a variable force is exerted upon said spacecraft by said tether, said force being offset from said center of mass. |
| 申请公布号 |
US2014166815(A1) |
申请公布日期 |
2014.06.19 |
| 申请号 |
US201314025822 |
申请日期 |
2013.09.13 |
| 申请人 |
DULA ARTHUR M. |
发明人 |
DULA ARTHUR M. |
| 分类号 |
B64G1/24 |
主分类号 |
B64G1/24 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A spacecraft reaction control system comprising:
a spacecraft having a center of mass; a length of free tether extending from said spacecraft and offset from said spacecraft's center of mass, such that a force exerted upon said spacecraft by said free tether will be offset from said spacecraft's center of mass.
|
| 地址 |
Houston TX US |
