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[1]刘锋,申智帅,王波,等.气动增压空间推进系统及相关技术试验研究[J].火箭推进,2017,43(06):38-43.
 LIU Feng,SHEN Zhishuai,et al.Experimental study on pneumatic pressurization space propulsion system and its correlation technology[J].Journal of Rocket Propulsion,2017,43(06):38-43.
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气动增压空间推进系统及相关技术试验研究

参考文献/References:

[1] 申智帅, 阮海军. 气动增压器技术及其在空间推进系统的应用[J]. 火箭推进, 2015, 41(3): 15-20.
SHEN Zhishuai, RUAN Haijun.Pneumopump technology and its applications in space propulsion system [J]. Journal of rocket propulsion, 2015, 41(3): 15-20.
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[3] 申智帅, 陈剑, 刘锋. 提高增压气温度对气动增压系统的影响分析[C]//中国航天第三专业信息网第三十六届学术交流会会议论文集. 银川:[出版者不详], 2015: 79-84.
[4] 申智帅, 刘锋, 魏彦祥. 气体性质对气动增压器性能的影响[J]. 火箭推进, 2014, 40(4): 50-54.
SHEN Zhishuai, LIU Feng, WEI Yanxiang.Influences of gas properties on pneumopump performance[J]. Journal of rocket propulsion, 2014, 40(4): 50-54.
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备注/Memo

收稿日期:2016-08-05
基金项目:上海市科学技术委员会资助项目(13DZ2250600)
作者简介: 刘锋(1971—),男,研究员,研究领域为液体火箭发动机系统设计

更新日期/Last Update: 1900-01-01