| 发明名称 |
CUBESAT FORM FACTOR THERMAL CONTROL LOUVERS |
| 摘要 |
Thermal control louvers for CubeSats or small spacecraft may include a plurality of springs attached to a back panel of the thermal control louvers. The thermal control louvers may also include a front panel, which includes at least two end panels interlocked with one or more middle panels. The front panel may secure the springs, shafts, and flaps to the back panel. |
| 申请公布号 |
US2017088294(A1) |
申请公布日期 |
2017.03.30 |
| 申请号 |
US201514867896 |
申请日期 |
2015.09.28 |
| 申请人 |
U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration |
发明人 |
WILLINGHAM ALLISON L. |
| 分类号 |
B64G1/50;E06B7/084 |
主分类号 |
B64G1/50 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. Thermal control louvers for a CubeSat or small spacecraft, comprising:
a plurality of springs attached to a back panel of the thermal control louvers; and a plurality of panels interlocking together to form a modular front panel, wherein the modular front panel secures the plurality of springs, a plurality of shafts, and a plurality of flaps to the back panel. |
| 地址 |
Washington DC US |
