摘要
文章介绍了一种典型的倒拉式回收降落伞伞包的受力情况分析和计算方法。该方法通过取用某一型号伞包设计参数进行计算 ,所得结果与实际情况比较符合。
The method used for analysis and prediction the loads of a typical parachute is introduced. By using this method to calculate the stretch force of parachute bag with the design parameters of a given project, the results accord with the practical situation of a real space vehicle.
出处
《航天返回与遥感》
2005年第1期14-17,共4页
Spacecraft Recovery & Remote Sensing
关键词
回收
降落伞
伞包
Recovery Parachute Parachutes Bag
