“天问一号”火星探测中的大折展比形状记忆可展开子系统
曾成均 , 刘立武 , 杜洋 , 于淼 , 辛晓洲 , 刘天珍 , 许培磊 , 闫俣 , 张豆 , 戴雯煦 , 兰鑫 , 张风华 , 王林林 , 万雪 , 边文凤 , 刘彦菊 , 冷劲松
Engineering ›› 2023, Vol. 28 ›› Issue (9) : 49 -57.
“天问一号”火星探测中的大折展比形状记忆可展开子系统
A Shape-Memory Deployable Subsystem with a Large Folding Ratio in China’s Tianwen-1 Mars Exploration Mission
Once China’s Tianwen-1 Mars probe arrived in a Mars orbit after a seven-month flight in the deep cold space environment, it would be urgently necessary to monitor its state and the surrounding environment. To address this issue, we developed a flexible deployable subsystem based on shape memory polymer composites (SMPC-FDS) with a large folding ratio, which incorporates a camera and two temperature telemetry points for monitoring the local state of the Mars orbiter and the deep space environment. Here, we report on the development, testing, and successful application of the SMPC-FDS. Before reaching its Mars remote-sensing orbit, the SMPC-FDS is designed to be in a folded state with high stiffness; after reaching orbit, it is in a deployed state with a large envelope. The transition from the folded state to the deployed state is achieved by electrically heating the shape memory polymer composites (SMPCs); during this process, the camera on the SMPC-FDS can capture the local state of the orbiter from multiple angles. Moreover, temperature telemetry points on the SMPC-FDS provide feedback on the environment temperature and the temperature change of the SMPCs during the energization process. By simulating a Mars on-orbit space environment, the engineering reliability of the SMPC-FDS was comprehensively verified in terms of the material properties, structural dynamic performance, and thermal vacuum deployment feasibility. Since the launch of Tianwen-1 on 23 July 2020, scientific data on the temperature environment around Tianwen-1 has been successfully acquired from the telemetry points on the SMPC-FDS, and the local state of the orbiter has been photographed in orbit, showing the national flag of China fixed on the orbiter.
空间可展开结构 / 形状记忆聚合物复合材料 / 火星探测 / 温度遥测 / 在轨展开
Flexible deployable structure / Shape memory polymer composite / Mars exploration / Temperature telemetry / On-orbit deployment
/
| 〈 |
|
〉 |