| 发明名称 |
Deployable Device for the Thermal Insulation of Cryonic Tanks of Spacecraft |
| 摘要 |
In a deployable device for the thermal insulation of cryogenic tanks (2) of spacecraft (1), including at least one insulating mat (8), preferably a plurality of insulating mats (8) distributedly arranged in the peripheral direction of the tank, and deployment means each associated to the insulating mat(s) (8) for unrolling the insulating mat(s) (8) from the rolled-up state into the extended state, the deployment means comprises at least one shape-changing element (7) extending in the unrolling direction, which is connected to, or integrated with, the insulating mat (8) and capable of being unrolled from the rolled-up state into the extended state by a controlled change in shape. |
| 申请公布号 |
US2016297552(A1) |
申请公布日期 |
2016.10.13 |
| 申请号 |
US201615094322 |
申请日期 |
2016.04.08 |
| 申请人 |
RUAG Space GmbH |
发明人 |
MOSER Martin;HOIDN Walter |
| 分类号 |
B64G1/58;B64G1/40;B64G1/22 |
主分类号 |
B64G1/58 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A deployable device for the thermal insulation of cryogenic tanks of spacecraft, including at least one insulating mat, preferably a plurality of insulating mats distributedly arranged in the peripheral direction of the tank, and deployment means each associated to the insulating mat(s) for unrolling the insulating mat(s) from the rolled-up state into the extended state, characterized in that the deployment means comprises at least one shape-changing element (7) extending in the unrolling direction, which is connected to, or integrated with, the insulating mat (8) and capable of being unrolled from the rolled-up state into the extended state by a controlled change in shape. |
| 地址 |
Vienna AT |
