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研究应变测试方法和太空船在热力场中的精度评估
Bo Zang1, Baokang Zhang1, Yuhan Liu1
1Beijing Institute of Space Mechanics & Electricity, Beijing, China.
Science progress
|June 11, 2024
概括
本研究提出了一种新的实验方法,用于模拟航天器结构上的联合力和热场. 验证的技术确保航天器的结构完整性符合飞行要求.
科学领域:
- 航空航天工程 航空航天工程
- 材料科学 材料科学 材料科学
- 结构分析 结构分析
背景情况:
- 实地实验对于验证航天器结构性能和质量至关重要.
- 模拟联合飞行力和热场在实验设计中构成了重大挑战.
研究的目的:
- 为了研究一个静态强度实验方法,用于在联合力和热场下的航天器.
- 开发和验证用于现实的飞行条件的模拟方法.
主要方法:
- 使用安全气囊来模拟力场.
- 使用电阻加热器来模拟热场.
- 在合环境条件下对静态强度测试进行了调查.
主要成果:
- 成功模拟了太空飞船飞行代表的联合力和热场.
- 拟议的实验方法显示出高精度.
- 验证了航天器的结构强度在飞行过程中符合技术要求.
结论:
- 开发的实验方法准确模拟了联合力和热场.
- 该方法验证了航天器在飞行条件下的结构强度.
- 这种方法提高了航天器结构验证的可靠性.
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