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Analysis of Reliability Evaluation Method of Reusable Liquid Rocket Engine
- GA Yongjing, LI Wenzhao, SONG Qianqiang, CHU Liang, MA Yitong, XIE Shuang, SHEN Bo
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Beijing Institute of Astronautical Systems Engineering, Beijing 10076, China
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Received |
Revised |
Published |
21 Apr 2022 |
19 May 2022 |
06 Jan 2023 |
Issue Date |
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20 Oct 2022 |
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References
[1] 龙乐豪,王国庆,吴宝胜,等. 我国重复使用航天运输系统发展现状及展望[J]. 国际太空,2019(9):4-10
[2] 杨勇,王小军,唐一华,等. 重复使用运载器发展趋势及特点[J]. 导弹与航天运载技术,2002(5):15-19
YANG Y,WANG X J,TANG Y H,et al. Development trends and characteristics of reusable launch vehicles[J]. Missiles and Space Vehicles,2002(5):15-19
[3] 郑孟伟,岳文龙,孙纪国,等. 我国大推力氢氧发动机发展思考[J]. 宇航总体技术,2019,3(2):12-17
ZHENG M W,YUE W L,SUN J G,et al. Discussion on Chinese large-thrust hydrogen-oxygen rocket engine development[J]. Astronautical System Engineering Technology,2019,3(2):12-17
[4] 汪钺. 航天飞机主发动机的可靠性是怎样获得的[J]. 国外导弹与宇航,1982(1):37-40
[5] 潘勇,黄进永,胡宁 . 可靠性概论[M]. 北京:电子工业出版社出版,2015.
[6] 宋征宇,方志耕,赫武乐,等. 基于贝叶斯理论的小子样运载火箭可靠性评估技术[J]. 深空探测学报(中英文),2021,8(1):62-69
SONG Z Y,FANG ZH G,HE W L,et al. Research on launch vehicle reliability assesement of small sample based on Bayes theory[J]. Journal of Deep Space Exploration,2021,8(1):62-69
[7] 闻悦,马婷婷,郑平军,等. 重复使用航天运输系统设计与评估[J]. 科学通报,2020,65(9):764-770
YUE W,MA T T,ZHEN P J,et al. Design and assessment of reusable space transportation system[J]. Chinese Science Bulletin,2020,65(9):764-770
[8] 孙国庆. 航天飞机主发动机试验[J]. 国外导弹技术,1980(7):20-27
[9] JOHNSON J R,COLBO H I. Space shuttle main engine progress through the first flight[C]//The 17th AIAA Joint Propulsion Conference. Colorado:Springs,1981.
[10] 谭松林,李宝盛. 液体火箭发动机可靠性[M]. 北京:中国宇航出版社,2014.
[11] 刘洪坤,王维彬. 发动机启动燃气反腔仿真与影响分析[J]. 火箭推进,2011,37(2):30-37
LIU H K,WANG W B. Backflow simulation and its influence analysis for gas generator of LRE[J]. Journal of Rocket Propulsion,2011,37(2):30-37
[12] 张楠,孙慧娟. 低温液体火箭发动机重复使用技术分析[J]. 火箭推进,2020,46(6):1-10
ZHANG N,SUN H J. Analysis on the reusable cryogenic liquid rocket engine technology[J]. Journal of Rocket Propulsion,2020,46(6):1-10
[13] BORIS I K,VLADIMIR K C,FELIX J C. Oxidizer-rich staged combustion rocket engines use and development in Russia[C]//AIAA Space Programs and Technologies Conference. Huntsville,AL:AIAA,1995.
[14] LACEFIELD T C,SPROW W J. High performance Russian NK-33 LOX/Kerosene liquid rocket engine[C]//The 30th AIAA Joint Propulsion Conference. Indianapolis,IN:AIAA,1994.
[15] 徐浩海,刘站国. 补燃循环发动机启动过程涡轮功率控制[J]. 火箭推进,2006,32(4):10-14
XU H H,LIU Z G. Turbine power control of staged combustion cycle engine during start-up[J]. Journal of Rocket Propulsion,2006,32(4):10-14
[16] 王珏,孙慧娟,刘恒,等. 膨胀循环发动机低温启动特性研究[J]. 导弹与航天运载技术,2021(6):7-11
WANG J,SUN H J,LIU H,et al. Research on the start-up characteristics of expander cycle engine with a colder thrust chamber[J]. Missiles and Space Vehicles,2021(6):7-11
[17] BINDER M P. A transient model of the RL10A-3-3A rocket engine[C]//The 31st AIAA Joint Propulsion Conference and Exhibit. San Diego,CA:AIAA,1995.
[18] BINDER M P. RL10A-3-3A rocket engine modeling project:NASA-TM-107318[R]. Washington DC:NASA,1997.
[19] 袁洁,潘亮. 基于发动机试车时序的某钝感点火器燃烧时间可靠性评估[J]. 火箭推进,2015,41(3):87-97
YUAN J,PAN L. Reliability assessment of a certain insensitive igniter based on start-up time-sequence of rocket engine[J]. Journal of Rocket Propulsion,2015,41(3):87-97
[20] 刘杰,王普,刘炳章. 最大熵试验法及其应用[J]. 自动化学报,2007,33(11):1226-1228
LIU J,WANG P,LIU B Z. Test method with the maximum entropy and its application[J]. Acta Automatica Sinical,2007,33(11):1226-1228
[21] 刘炳章,丁同才. 小子样验证高可靠性的可靠性评估方法及其应用[J]. 质量与可靠性,2004(1):19-22
[22] 董海平,柳洋,袁世越. 基于正态容许限法的点火器可靠性评估[J]. 科技创新导报,2021(4):5-9.
DONG H P,LIU Y,YUAN S Y. Reliability evaluation of igniter based on normal allowable limit method[J]. Science and Technology Innovation Herald,2021(4):5-9.