| 摘要: |
| 通过对火箭发动机－超音速扩压器－蒸汽引射泵组合式高空模拟系统的理论分析和实验研究，提出了扩大ＧＳ－１高空模拟试车台试验能力的几项新方案。 |
| 关键词: 液体推进剂火箭发动机 高空试验 试验设备 超音速扩压器 |
| DOI： |
| 分类号:V433.9 |
| 基金项目: |
|
| A STUDY ON PERFORMANCES OF HIGH ALTITUDE SIMULATION TEST SYSTEM COMPOSED OF ROCKET ENGINE, SUPERSONIC DIFFUSER AND VAPOUR JET VACUUM PUMP |
|
Zhang Kuihao
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Zhang Kuihao(The 101st Research Inst., Beijing, 100074
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| Abstract: |
| In this paper, high altitude simulation test system composed of rocket engine, supersonic diffuser and vapour jet vacuum pump is analysed theoretically and studied experimentally. Several new methods used to extend test ability of GS-1 High Altitude Simulation Test Bed are proposed. |
| Key words: Liquid propellant rocket engine High altitude test f Test equipment Supersonic diffuser |
