航天器展开机构转动阻尼器仿真分析与试验研究 / Simulation analysis and tests of rotating damper for spacecraft deployment mechanism
- Resource Type
- Academic Journal
- Source
- 振动与冲击 / Journal of Vibration and Shock. 42(13):310-315
- Subject
展开机构 转动阻尼器 阻尼力矩 阻尼率 deployment mechanism rotating damper damping torque damping rate - Language
- Chinese
- ISSN
- 1000-3835