| 火箭发动机－超音速扩压器－蒸汽引射泵组合式高空模拟试验系统的性能研究 |
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| 引用本文： | 张奎好. 火箭发动机－超音速扩压器－蒸汽引射泵组合式高空模拟试验系统的性能研究[J]. 推进技术, 1995, 16(2): 73-79 |
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| 作者姓名： | 张奎好 |
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| 作者单位： | 航天工业总公司１０１所 |
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| 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。
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| 关 键 词： | 液体推进剂 火箭发动机 高空试验 超音速扩压器 |
A STUDY ON PERFORMANCES OF HIGH ALTITUDE SIMULATION TEST SYSTEM COMPOSED OF ROCKET ENGINE, SUPERSONIC DIFFUSER AND VAPOUR JET VACUUM PUMP |
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| Zhang Kuihao. A STUDY ON PERFORMANCES OF HIGH ALTITUDE SIMULATION TEST SYSTEM COMPOSED OF ROCKET ENGINE, SUPERSONIC DIFFUSER AND VAPOUR JET VACUUM PUMP[J]. Journal of Propulsion Technology, 1995, 16(2): 73-79 |
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| Authors: | Zhang Kuihao |
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| Affiliation: | 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. |
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| Keywords: | Liquid propellant rocket engine High altitude test f Test equipment Supersonic diffuser |
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