Open Access
Issue |
JNWPU
Volume 41, Number 3, June 2023
|
|
---|---|---|
Page(s) | 626 - 634 | |
DOI | https://doi.org/10.1051/jnwpu/20234130626 | |
Published online | 01 August 2023 |
- WANG Jixiang, ZHANG Zhenhua, WANG Danyang. The world book of space launch vehicles[M]. Beijing: China Astronautic Publishing House, 1996: 382–383 (in Chinese) [Google Scholar]
- ZHANG Zhi. Review and prospect of manned launch vehicle technology[J]. Astronautical Systems Engineering Technology, 2018, 2(2): 56–61. [Article] (in Chinese) [Google Scholar]
- WU Xinfeng, PENG Qibo, ZHANG Hailian, et al. Analysis and thinking on the development of manned launch vehicles at home and abroad[J]. Manned Aerospace, 2020(6): 783–793. [Article] (in Chinese) [Google Scholar]
- WANG Xiaojun, XU Lijie. Research on the development of China's new generation medium high orbit launch vehicle[J]. General Technology of Aerospace, 2019, 3(5): 1–9. [Article] (in Chinese) [Google Scholar]
- LONG Lehao, ZHENG Liwei. Reflections on some problems of heavy launch vehicles[J]. General Technology of Aerospace, 2017, 1(1): 8–12. [Article] (in Chinese) [Google Scholar]
- LIU Jiajia, YAN Baofeng, BI Yongtao, et al. Some thoughts on the development of commercial small rockets[J]. General Aerospace Technology, 2018, 2(5): 65–70. [Article] (in Chinese) [Google Scholar]
- QIN Xudong, RONG Yi, WANG Xiaojun, et al. Analysis on the future development trend of China's launch vehicles based on generational research[J]. Missiles and Space Vehicles, 2014, 1: 1–4. [Article] (in Chinese) [Google Scholar]
- SHEN Chibing. Analysis of the influence of propellant utilization system on the performance of liquid-propellant rocket[J]. Propulsion Technology, 1997, 18(6): 6. [Article] (in Chinese) [Google Scholar]
- ZHOU Yaqiang, LOU Luliang, MOU Yu. Analysis on change of carrying capacity of typical launch vehicles at home and abroad[J]. Manned Aerospace, 2017, 23(6): 737–742. [Article] (in Chinese) [Google Scholar]
- ABRAMS I J. Optimum selection of fuel bias for maximizing the range and for minimizing the residual propellant of the Thor, Atlas and Titan missiles[J]. Planetary and Space Science, 1961, 4(1): 34–44 [NASA ADS] [CrossRef] [Google Scholar]
- CHEN Shiqiang, HUANG Hui, SHAO Yetao, et al. Reflections on the future demand direction and development suggestions of aerospace power system[J]. Astronautical Systems Engineering Technology, 2019, 3(1): 62–70. [Article] (in Chinese) [Google Scholar]
- NICHOLS R H. Saturn S-Ⅳ cryogenic weigh system part Ⅰ: propellant utilization[J]. IEEE Trans on Aerospace, 1965, AS-3(2): 144–151 [CrossRef] [Google Scholar]
- DODGE F T. Propellant mass gauging: database of vehicle applications and research and development studies[R]. NASA/CR-215281, 2008 [Google Scholar]
- SZABO S V, BERNS JR JAMES A, STOFAN A J. Centaur launch vehicle propellant utilization system[R]. NASA TND-4848, 1958 [Google Scholar]
- MAGRINI O J. Analysis of centaur propellant utilization difference bridge[R]. NASA TM X-1440, 1958 [Google Scholar]
- GE Lihu, ZOU Peihua. Application of propellant utilization system in foreign models[J]. World Missiles and Aerospace, 1987, 11: 43–48. [Article] (in Chinese) [Google Scholar]
- LONG Lehao. Overall design(I)[M]. Beijing: China Astronautic Publishing House, 1989 (in Chinese) [Google Scholar]
- LI Dong, WANG Jue, LI Pingqi, et al. Long March 5, China's new generation of large carrier rocket, achieved great success in its first flight[J]. International space, 2016(11): 1–7. [Article] (in Chinese) [Google Scholar]
- LI Dong, WANG Jue, HE Wei, et al. The overall scheme and key technologies of Long March 5 launch vehicle[J]. Missile and Aerospace Carrier Technology, 2017(3): 1–5. [Article] (in Chinese) [Google Scholar]
- LONG Lehao, ZHENG Liwei. Thoughts on some problems of heavy launch vehicle[J]. Astronautical Systems Engineering Technology, 2017, 1(1): 8–12. [Article] (in Chinese) [Google Scholar]
- LIU Zhusheng, ZHANG Borong. Development and prospect of multidisciplinary optimization methods for launch vehicle overall design[J]. Astronautical Systems Engineering Technology, 2017, 1(2): 1–6. [Article] (in Chinese) [Google Scholar]
- LONG Lehao, LI pingqi, QIN Xudong, et al. Review of the development of China's space transportation system in the past 60 years[J]. Overall Space Technology, 2018, 2(2): 1–6. [Article] (in Chinese) [Google Scholar]
- YU Menglun. Some reviews of the overall scheme demonstration of large-scale carrier in the 1990s[J]. Astronautical Systems Engineering Technology, 2018, 2(2): 7–16. [Article] (in Chinese) [Google Scholar]
- ZHENG Mengwei, YUE Wenlong, SUN Jiguo, et al. Thoughts on the development of high thrust oxyhydrogen engine in China[J]. Astronautical Systems Engineering Technology, 2019, 3(2): 12–17. [Article] (in Chinese) [Google Scholar]
- LIU Bing, LI Dong. Research on variable threshold control method for propellant utilization system of launch vehicles[J]. Missile and Aerospace Launch Technology, 2021(3): 1–5. [Article] (in Chinese) [Google Scholar]
- GAO Chen, LIU Bolong, LIU Yang, et al. Design and application of simulation platform for cryogenic propellant utilization system[J]. Missile and Aerospace Delivery Technology, 2019(4): 43–51. [Article] (in Chinese) [Google Scholar]
- LI Qiang, LI Guoai, MOU Yu. Modeling and simulation of propellant utilization system of launch vehicle[J]. Missiles and Space Vehicles, 2013(5): 32–36. [Article] (in Chinese) [Google Scholar]
- WEI Jiang, HUI Li, TAO Huanmei. The simulation of launch vehicle propellant-utilization system[C]//International Conference on Mechatronics and Automation, 2006 (in Chinese) [Google Scholar]
- SONG E J, CHO S, ROH W R. Optimal selection of fuel bias and propellant residual analysis of a liquid rocket[J]. Journal of the Korean Society for Aeronautical and Space Sciences, 2015, 43(1): 88–95 [NASA ADS] [Google Scholar]
- SUTTON G P. Rocket propulsion elements[M]. >7th ed. New Jersey: John Wiley & Sons, Inc. Hoboken [Google Scholar]
- HAN Hongwei, WANG Yijie. Study on the factors affecting the mixing ratio of liquid rocket engines[J]. Missiles and Space Vehicles, 2022(1): 36–40. [Article] (in Chinese) [Google Scholar]
- FU Quanjun. Current status and future development trend of liquid propellant[J]. Journal of Rocket Propulsion, 2004(1): 6. [Article] (in Chinese) [Google Scholar]
- ZHANG Qiyuan. Development and current situation of foreign liquid propellant[J]. Foreign Missiles and Aerospace, 1980(9): 9–17. [Article] (in Chinese) [Google Scholar]
- LIU Hongjun. Research on nonlinear adjustment of thrust and mixing ratio of liquid oxygen/kerosene rocket engine[J]. Propulsion Technology, 1998, 19(4): 4. [Article] (in Chinese) [Google Scholar]
- HUA Di, CHEN Zhao. Discussion on propellant safety margin[J]. Acta Aeronautica Sinica, 1979(4): 37–52 (in Chinese) [Google Scholar]
- CHEN Jianhua, CAO Chen, YANG Yongqiang. General technology of liquid oxygen kerosene engine of "Long March 5" rocket[J]. Journal of Deep Space Exploration, 2021, 8(4): 354–361. [Article] (in Chinese) [Google Scholar]
- WANG Weibin, GONG Yanbo. Design and development of a 50 ton hydrogen oxygen rocket engine[J]. Propulsion Technology, 2021, 42(7): 8. [Article] (in Chinese) [Google Scholar]
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