Open Access
Issue
JNWPU
Volume 40, Number 4, August 2022
Page(s) 723 - 731
DOI https://doi.org/10.1051/jnwpu/20224040723
Published online 30 September 2022
  1. ZHANG Lüyun, QU Jing, LONG Xuedan, et al. Review of world launch vehicle in 2018[J]. Missiles and Space Vehicles, 2019(1): 36–39 [Article] (in Chinese) [Google Scholar]
  2. ZHU Kun, YANG Tiecheng, ZHOU Ning. Discussion on the development route of space vehicle technology from the perspective of low cost[J]. Aerodynamic Missile Journal, 2021(6): 1–6 [Article] (in Chinese) [Google Scholar]
  3. HELLMAN B M, BRADFORD J E, GERMAIN B D S, et al. Two stage to orbit conceptual vehicle designs using the SABRE engine[C]//AIAA SPACE 2016, 2016 [Google Scholar]
  4. ZHAO Guozhu, HUANG Changmei, KANG Kaihua, et al. Development analysis of russian space launch vehicle technology in 2019[J]. Aerodynamic Missile Journal, 2020(2): 1–5 [Article] (in Chinese) [Google Scholar]
  5. TAN Yonghua, ZHAO Jian, CHEN Jianhua, et al. Progress in technology of main liquid rocket engines of launch vehicles in China[J]. Aerospace China, 2020, 21(2): 23–30 (in Chinese) [Google Scholar]
  6. ZHENG Mengwei, YUE Wenlong, SUN Jiguo, et al. Development of high-thrust hydrogen-oxygen engine in china[J]. Journal of Aerospace Engineering, 2019, 3(2): 12–17 (in Chinese) [Google Scholar]
  7. LI Bin, ZHANG Xiaoping, GAO Yushan. Thinking on the development of reusable liquid rocket engine in China[J]. Journal of Rocket Propulsion, 2017, 43(1): 7 [Article] (in Chinese) [Google Scholar]
  8. HAN Wei. Numerical study on coupled heat transfer in regenerative cooling thrust chamber of liquid rocket engine[D]. Harbin: Harbin Engineering University, 2017 (in Chinese) [Google Scholar]
  9. YU Zhonghao, JIN Ping, CAI Guobiao. Influence of design parameters of reusable liquid rocket engine on ratchet strain of thrust chamber body[J]. Manned Space Flight, 2018, 24(2): 8 [Article] (in Chinese) [Google Scholar]
  10. SUN Bing, DING Zhaobo, KANG Yudong. Life prediction of liquid rocket engine thrust chamber liner wall[J]. Journal of Aerospace Power, 2014, 29(12): 2980–2986 [Article] (in Chinese) [Google Scholar]
  11. SUN Bing, SONG Jiawen. Coupled heat transfer characteristics of step cooling channel for liquid oxygen methane engine[J]. Journal of Aerospace Power, 2016, 31(12): 2972–2978 [Article] (in Chinese) [Google Scholar]
  12. SUN Bing, SONG Jiawen. Three-dimensional thermal structure analysis of liquid rocket engine thrust chamber wall under transient loading[J]. Journal of Propulsion Technology, 2016, 37(7): 1328–1333 [Article] (in Chinese) [Google Scholar]
  13. SONG Jiawen, SUN Bing. Thermal-structural analysis of regeneratively-cooled thrust chamber wall in reusable LOX/Methane rocket engines[J]. Chinese Journal of Aeronautics, 2017, 30(3): 1043–1053 [Article] [CrossRef] [Google Scholar]
  14. DI L A, BING S A, TW A, et al. Thermo-structural analysis of regenerative cooling thrust chamber cylinder segment based on experimental data[J]. Chinese Journal of Aeronautics, 2020, 33(1): 102–115 [Article] [CrossRef] [Google Scholar]
  15. PIZZARELLI M. Correction: an algebraic model for structural and life analysis of regeneratively-cooled thrust chambers[J]. Journal of Propulsion and Power, 2020, 36(6): 191–201 [CrossRef] [Google Scholar]
  16. RICCIUS J R, BTTCHER M W. A first step into the blanching modelling of liquid rocket engines: taking into account the roughness increase of the chamber wall[C]//AIAA Propulsion and Energy 2019 Forum, 2019 [Google Scholar]
  17. ESPOSITO J J, ZABORA R F. Thrust chamber life prediction. Volume 1: mechanical and physical properties of high performance rocket nozzle materials[R]. NASA-CR-134806, 1975 [Google Scholar]
  18. ELLIS D L, MICHAL G M. Mechanical and thermal properties of two Cu-Cr-Nb alloys and NARloy-Z[R]. NASA-CR-198529, 1996 [Google Scholar]

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