激波风洞两级入轨飞行器纵向级间分离试验技术 / Test technology of longitudinal stage separation for two-stage-to-orbit vehicle in shock tunnel
- Resource Type
- Academic Journal
- Source
- 航空学报 / Acta Aeronautica ET Astronautica Sinica. 44(17):103-121
- Subject
两级入轨 多体分离 高超声速 级间分离 轨迹捕获 激波风洞 two stages to orbit(TSTO) multi-body separation hypersonic stage separation trajectory capture shock tunnel - Language
- Chinese
- ISSN
- 1000-6893