|Table of Contents|

Development of propulsion technology for Chinese manned launch vehicles(PDF)

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

Issue:
2011年02期
Page:
1-7
Research Field:
专论与综述
Publishing date:

Info

Title:
Development of propulsion technology for Chinese manned launch vehicles
Author(s):
LI Ping
Xi’an Aerospace Propulsion Institute, Xi’an 710100, China
Keywords:
manned spaceflight;  launch vehicle;  liquid rocket engine;  propulsion technology
PACS:
V434-34
DOI:
-
Abstract:
The history and newly progress of main space powers in the area of space launch vehicles and their propulsion technologies are reviewed. The state-of-art and future developing ideas of propulsion technologies in the United States and Russia are analyzed emphatically. Comparing with differential technologies and propulsion levels of current popular launch vehicles, the developing trends of world space launch vehicles and their propulsion systems are summarized, and suggestions on developing advanced propulsion technologies for Chinese manned spaceflight launch vehicles are made.

References:

[1]SUTTON George P, EDWARDS Tim. Propulsion and power history of US and USSR[J]. Journal of Propulsion and Power, 2006, 30: 1-6.
[2]CAVENY L H. Solid rocket enabling technologies and milestones in the United States[J]. Journal of Propulsion and Power, 2003, 27: 7-14.
[3]李东, 程堂明. 中国新一代运载火箭发展展望[J]. 中国航天, 2008 (2): 13-16.
[4]李平, 葛明龙, 李楚林. 欧洲航天动力规划与中国空间推进技术发展对策[J]. 火箭推进, 2003 (3).
[5]张小平, 李斌. 中国下一代航天主动力--大推力液氧煤油发动机研究[C]//中国航天第三专业信息网第31届技术交流会文集，2010, 8.
[6]龙乐豪. 中国航天运输系统发展展望[J]. 航天制造技术, 2010 (3): 5-10.

Memo

Memo:
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Last Update: 1900-01-01