|Table of Contents|

Analysis of technologies for space transportation in consideration of cost(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2013年01期
Page:
8-14
Research Field:
研究与设计
Publishing date:

Info

Title:
Analysis of technologies for space transportation in consideration of cost
Author(s):
JIN Xiao-wei;  LI Ping;  LIU Chang-an;  MA Jian
Xi’an Aerospace Propulsion Institute, Xi’an 710100, China
Keywords:
space transportation;  SSTO;  TSTO;  air launch;  combined cycle
PACS:
V434-34
DOI:
-
Abstract:
The factors affecting the cost of space transportation is analyzed with the energy analysis method. The injection orbit mode, launch method and propulsion system are analyzed emphatically. The development way of the space transportation technologies in future is proposed in this paper.

References:

[1]KETSDEVER A D, YOUNG M P, MOSSMAN J B, et al. Overview of advanced concepts for space access[J]. Jour- nal of Spacecraft and Rockets, 2010, 47(2): 239-240.
[2]朱森元. 论单级入轨火箭运载器的发展途径[J]. 导弹与航天运载技术, 2002 (5): 11-14.
[3]余梦伦. 两级入轨重复使用运载器的方案探讨[J]. 装备指挥技术学院学报, 2006, 17(1): 1-5.
[4]SARIGUL-KLIJN M, SARIGUL-KLIJN N. A study of air launch methods for RLVs, AIAA 2001-4619[R]. USA: AIAA, 2001.
[5]王晓青, 王小军, 王国辉. 空射运载火箭方案研究[J]. 导弹与航天运载技术, 2008 (3): 1-5.
[6]张蒙正, 李平, 陈祖奎. 组合循环动力系统面临的挑战及前景[J]. 火箭推进, 2009, 35(1): 1-8.
[7]果琳丽, 朱永贵. 空间站天地往返运输系统初探[J]. 导弹与航天运载技术, 2000 (1): 7-11.
[8]DISSEL A F, KOTHARI A P, RAGHAVAN V. System analysis of launch transportation options for crew explo- ration vehicle, AIAA 2005-4366[R]. USA：AIAA，2005.
[9]DISSEL A F, KOTHARI A P, LEWIS M J. Weight growth study of reusable launch vehicle systems, AIAA 2005-4369[R]. USA: AIAA, 2005.
[10]KOTHARI A P, LIVINGSTON J W，TARPLEY C. Rocket based combined cycle hypersonic vehicle design for or- bital access, AIAA 2010-2338[R]. USA：AIAA, 2010.
[11]KOTHARI A P, LIVINGSTON J W, TARPLEY C. A reusable, rocket and airbreathing combined cycle hyper- sonic vehicle design for access-to-space, AIAA 2010-8905[R]. USA: AIAA, 2010.
[12]朱森元.单级入轨运输器的发射技术研究[J]. 导弹与航天运载技术, 2001 (5): 1-5.
[13]陈宏, 何国强. RBCC和TBCC组合发动机在RLV上的应用[J]. 火箭推进, 2008 (3): 39-43.
[14]詹浩, 孙得川, 邓阳平. 基于RBCC的天地往返运载器动力方案研究[J]. 固体火箭技术, 2008 (4): 353-357.

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Last Update: 1900-01-01