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液体运载火箭交叉输送总体参数研究 被引量:11

Study on System Parameters of Cross-feed Technology in Liquid Rocket
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摘要 交叉输送是指飞行中将一个贮箱内推进剂输送到另一个贮箱内的技术,它能提高液体捆绑火箭运载能力和可靠性。以某重型火箭为对象,对交叉输送总体参数进行了研究,包括运载能力贡献、输送能源、增压、出流参数以及晃动特性。研究表明:助推-芯级宜采用重力输送方式,此时助推-助推贮箱间推进剂晃动周期约30 s,初始液位差将缓慢地达到平衡,对火箭总体运动无影响。 Cross-Feed is a technology that feeds propellant from one tank to another. It can be used to improve the launch capability and reliability of liquid cluster rocket. The system parameters of this technology, including the launch capability, feed energy, pressurization, outflow, as well as slosh behaviors, are researched for a certain heavy rocket. We found that the gravity-feed is preferred in feeding the propellant of booster to the stage-1. The slosh period between each booster is about 30 seconds, and the initial height difference of propellants will be eliminated slowly. This movement will not influence the motion of the rocket.
作者 汤波 胡久辉 邵业涛 黄辉 Tang Bo Hu Jiu-hui Shao Ye-tao Huang Hui(Beijing Institute of Astronautical System Engineering, Beijing, 100076)
出处 《导弹与航天运载技术》 CSCD 北大核心 2017年第3期22-27,共6页 Missiles and Space Vehicles
关键词 交叉输送 运载能力 输送能源 晃动 Cross-feed Launch capability Feed energy Slosh
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  • 1廖少英,顾仁年.新一代运载火箭增压输送系统交叉输送技术研究[J].上海航天,2005,22(3):37-41. 被引量:12
  • 2Laurini K,Hufenbach B,Schade B.From LEO,to the Moon,then Mars:Developing a global strategy for exploration risk reduction[R].IAC-09-B3 -1.7,2009.
  • 3Donahue B,Graham N,Lizenby J,et al.An additional space exploration mission opportunity for the Ares-V launch system[R] ,IAC-09-D2.8.4,2009.
  • 4MARTIN J A. Two-stage earth-to-orbit vehicles with series and parallel burn[R]. AIAA-86-1413, 1986.
  • 5MARSHALL W R. Three stage rocket vehicle with parallel staging[R]. NASA, N83-12138.
  • 6NEWTON K E. Atlas/Centaur Launch Vehicle [ R].SAE 680737.
  • 7Saturn V flight manual SA507 [M]. NASA, TM-X 62634.
  • 8GILMORE W L. Supplying cryogenic propellants for space based OTV[R]. AIAA-85-5256.
  • 9Press information space shuttle transportation system [R]. E 30277-u, 1980.
  • 10SOUCHIER A, PASQUIER J. Ariane 4 liquid boosters and first stage propulsion system[R]. AIAA-83-1192.

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