| Citation: | CHEN Qiang, SUN Qingguo, WANG Tianxiang. Liquid methane subcooling and filling process using liquid nitrogen as cold source[J]. Journal of Aerospace Power, 2020, 35(5): 956-962. doi: 10.13224/j.cnki.jasp.2020.05.007
|
| [1] |
曾占魁,史敏辉.国内商业航天机构调研分析［J］.中国航天,2018(1):11-15. ZENG Zhankui,SHI Minhui.Research and analysis of domestic commercial space agencies［J］.Aerospace China,2018(1):11-15.(in Chinese)
|
| [2] |
李文龙,李平,邹宇.烃类推进剂航天动力技术进展与展望未来［J］.宇航学报,2015,36(3):243-252. LI Wenlong,LI Ping,ZOU Yu.Review and future trend of space propulsion technique using hydrocarbon propellants［J］.Journal of Astronautics,2015,36(3):243-252.(in Chinese)
|
| [3] |
尹亮,刘伟强.液氧/甲烷发动机研究进展与技术展望［J］.航空兵器,2018(4):21-27. YIN Liang,LIU Weiqiang.Review and prospect of LOX/methane rocket engine systems［J］.Aero Weaponry,2018(4):21-27.(in Chinese)
|
| [4] |
郑大勇,颜勇,孙纪国.液氧甲烷发动机重复使用关键技术发展研究［J］.导弹与航天运载技术,2018(2):31-35. ZHENG Dayong,YAN Yong,SUN Jiguo.Development study of key reusable technology for LOX/methane engine［J］.Missiles and Space Vehicles,2018(2):31-35.(in Chinese)
|
| [5] |
符锡理.运载火箭液氢液氧低温推进剂加注技术［J］.低温工程,1995(6):1-8. FU Xili.A review of LH2,LO2 cryogenic propellant loading technology for launch vehicles［J］.Cryogenics,1995(6):1-8.(in Chinese)
|
| [6] |
王维彬,孙纪国.航天动力发展的生力军:液氧甲烷火箭发动机［J］.航天制造技术,2011(2):3-6. WANG Weibing,SUN Jiguo.Liquid oxygen and methane rocket engine:the new force of space power development［J］.Aerospace Manufacturing Technology,2011(2):3-6.(in Chinese)
|
| [7] |
孙宏明.液氧/甲烷发动机评述［J］.火箭推进,2006,32(2):23-31. SUN Hongming.Review of liquid oxygen/methane rocket engine［J］.Journal of Rocket Propulsion,2006,32(2):23-31.(in Chinese)
|
| [8] |
符锡理.土星I(SA-7)运载火箭液氢加注系统［J］.国外导弹与航天运载器,1987(2):60-64. FU Xili.Liquid hydrogen loading system of Saturn I (SA-7) launch vehicle［J］.Foreign Missiles and Space Vehicles,1987(2):60-64.(in Chinese)
|
| [9] |
符锡理.国外航天发射场液氢液氧加注系统［J］.国外导弹与航天运载器,1984(6):40-51. FU Xili.Liquid hydrogen and liquid oxygen filling system of foreign space launch sites［J］.Foreign Missiles and Space Vehicles,1984(6):40-51.(in Chinese)
|
| [10] |
符锡理.土星Ⅰ(SA-10)运载火箭37B发射场液氢加注系统［J］.国外导弹技术,1981(10):42-47. FU Xili.Liquid hydrogen filling system for 37B launch site of Saturn I (SA-10) launch vehicle［J］.Foreign Missiles Technology,1981(10):42-47.(in Chinese)
|
| [11] |
程水旺.日本运载火箭液氢地面贮存加注系统综述［J］.低温工程,1994(3):1-8. CHENG Shuiwang.A summary of the ground LH2 storing and fuelling system of the launch vehicles of Japan［J］.Cryogenics,1994(3):1-8.(in Chinese)
|
| [12] |
杨金宁.低温推进剂的温度控制［J］.低温工程,1994(1):17-21. YANG Jinning.Temperature control of the low temperature propellant［J］.Cryogenics,1994(1):17-21.(in Chinese)
|
| [13] |
王瑞铨.国外运载火箭低温加注系统［J］.导弹与航天运载技术,1997(2):21-31. WANG Ruiquan.The cryogenic fueling systems of foreign launch vehicles［J］.Missiles and Space Vehicles,1997(2):21-31.(in Chinese)
|
| [14] |
JOHNSON W L,TOMSIK T M,SMUDDE T D.A densified liquid methane delivery system for the Altair as-cent stage［R］.AIAA-2010-1904,2010.
|
| [15] |
MUSTAFI S,CANAVAN E,JOHNSON W.Subcooling cryogenic propellant for long duration space exploration［R］.AIAA-2009-6584,2009.
|
| [16] |
MUSTAFI S,JOHNSON W,KASHANI A.Subcooling for long duration in-space cryogenic propellant storage［R］.AIAA-2010-8869,2010.
|
| [17] |
TOMSIK T M,MEYER M L.Liquid oxygen propellant densification production and performance test results with a large-scale flight-weight propellant tank for the X33RLV［R］.NASA TM-216247,2010.
|
| [18] |
谢福寿,雷刚,王磊,等.过冷低温推进剂的性能优势及其应用前景［J］.西安交通大学学报,2015,49(5):16-23. XIE Fushou,LEI Gang,WANG Lei,et al.Performance advantages and application prospects of subcooled cryogenic propellants［J］.Journal of Xi’an Jiaotong University,2015,49(5):16-23.(in Chinese)
|
| [19] |
谢福寿,厉彦忠,王磊,等.低温推进剂过冷技术研究［J］.航空动力学报,2017,32(3):762-768. XIE Fushou,LI Yanzhong,WANG Lei,et.al.Study on subcooled technology for cryogenic propellants［J］.Journal of Aerospace Power,2017,32(3):762-768.(in Chinese)
|
| [20] |
邵业涛,罗庶,王浩苏,等.低温推进剂深度过冷加注技术研究及对运载火箭性能影响分析［J］.宇航总体技术,2019,3(2):18-25. SHAO Yetao,LUO Shu,WANG Haosu,et al.Research on the supercooling loading technology of cryogenic propellant and its effects on rocket performance［J］.Astronautical Systems Engineering Technology,2019,3(2):18-25.(in Chinese)
|
| [21] |
Space X Company.Falcon 9 user’s guide［EB/OL］.［2019-09-10］.https:∥www.spacex.com/sites/spacex/files/falcon_users_guide_10_2019.pdf.
|
| [22] |
胡旭东,宋扬.液氧全过冷加注在新一代运载火箭加注工作中的应用价值［J］.导弹与航天运载技术,2018(4):87-92. HU Xudong,SONG Yang.Application value analysis of subcooled liquid oxygen full loading in new generation of launch vehicles［J］.Missiles and Space Vehicles,2018(4):87-92.(in Chinese)
|
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