航天推进技术研究院主办
JIANG Ming-wei.Analysis of propellant refueling program for Russian Space Station[J].Journal of Rocket Propulsion,2013,39(04):8-12.
俄罗斯空间站推进剂补加程序分析
- Title:
- Analysis of propellant refueling program for Russian Space Station
- 文章编号:
- 1672-9374(2013)04-0008-05
- 分类号:
- V476-34
- 文献标志码:
- A
- 摘要:
- 补加程序是推进剂补加系统的关键技术之一,而目前也仅有俄罗斯有成功应用的经验。根据目前获取的资料,经过计算、仿真和论证,对俄罗斯空间站的补加系统进行了研究,分析了ATV对空间站进行推进剂补加的程序,初步得到了俄罗斯空间站推进剂补加的特点,可作为目前我国空间站方案论证期间补加程序的参考。
- Abstract:
- The refueling program is one of the key technologies of propellant refueling system, for which only Russians has succeeded in application until now. The refueling system of Russian Space Station was researched on the basis of material on hand, calculation, simulation and argumentation. The propellant refueling program of ATV for space station was analyzed in this paper. The propellant refueling program of Russian Space Station was preliminarily obtained, which can be used as a refe- rence during the scheme argumentation of refueling program for Chinese space station.
参考文献/References:
[1]臧家亮. 空间站及其推进系统[J]. 载人航天, 2003 (2): 29-36.
[2]KITMACHER G. Reference guide to the international space station[EB/OL]. (2006-08-20) [2010-09-25]. www.nasa.gov/pdf/508318main_ISS_ref_guide_nov2010.
[3]HARLAND D M. The story of space station MIR[M]. Germany: Springer, 2005.
[4]PORTREE D F S. MIR hardware HERITAGE[EB/OL]. [2012-04-16]. http://www. en.wikisource.org/wiki.
[5]BAYLE O, HULLIER V-L, GANET M, et al. Influence of the ATV propellant sloshing on the GNC performance, AIAA 2002-4845[R]. USA: AIAA, 2002.
[6]LAIN R, VERNE J. Automated transfer vehicle[R]. [S.l.]: ESA, 2005.
备注/Memo
收稿日期:2012-10-30;修回日期:2013-01-25
作者简介:江铭伟(1976—),男,高级工程师,研究领域为空间飞行器推进系统