航天推进技术研究院主办
[1]周利民,刘中祥.膨胀循环发动机技术的发展、应用与展望[J].火箭推进,2016,42(01):1-5.
ZHOU Limin,LIU Zhongxiang.Development, application, and prospect of expander cycle engine technology[J].Journal of Rocket Propulsion,2016,42(01):1-5.
点击复制
ZHOU Limin,LIU Zhongxiang.Development, application, and prospect of expander cycle engine technology[J].Journal of Rocket Propulsion,2016,42(01):1-5.
膨胀循环发动机技术的发展、应用与展望
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
42
期数:
2016年01期
页码:
1-5
栏目:
专论与综述
出版日期:
2016-04-01
- Title:
- Development, application, and prospect of expander cycle engine technology
- Keywords:
- expander cycle engine; rocket engine; technology development
- 分类号:
- V434-34
- 文献标志码:
- A
- 摘要:
- 系统总结了国内外膨胀循环发动机技术的发展和应用情况,在分析未来航天发展需求、研究膨胀循环发动机技术发展方向的基础上,对膨胀循环发动机技术未来的发展进行了展望.
相似文献/References:
[1]霍世慧,袁军社,徐学军,等.双推力室机架快速优化设计方法研究[J].火箭推进,2015,41(04):55.
HUO Shihui,YUAN Junshe,XU Xuejun,et al.A rapid optimization design method for frame structure
of double thrust chambers[J].Journal of Rocket Propulsion,2015,41(01):55.
[2]沈传兵,苏 杭,朱子勇.基于PLC和WinCC的火箭发动机热真空试验控制系统[J].火箭推进,2015,41(03):93.
SHEN Chuan-bing,SU Hang,ZHU Zi-yong.Control system for liquid rocket engine heat-vacuum
test based on PLC and WinCC[J].Journal of Rocket Propulsion,2015,41(01):93.
[3]周 伟.某膨胀循环发动机推力室冷却结构流场仿真分析[J].火箭推进,2015,41(02):63.
ZHOU Wei.Flow field simulation analysis of cooling configuration
in thrust chamber of an expander cycle engine[J].Journal of Rocket Propulsion,2015,41(01):63.
[4]刘万龙,牛向楠,李全令,等.一种姿轨控发动机地面试验控制系统设计[J].火箭推进,2015,41(02):114.
LIU Wan-long,NIU Xiang-nan,LI Quan-ling,et al.Design of a ground test control system for attitude
and orbital control engine[J].Journal of Rocket Propulsion,2015,41(01):114.
[5]段文浩,于 涛,杨 莹.辐射式热流测量系统及其应用[J].火箭推进,2014,40(01):85.
DUAN Wen-hao,YU Tao,YANG Ying.Radiant heat flux measuring system and its application[J].Journal of Rocket Propulsion,2014,40(01):85.
[6]朱子环,耿卫国,管 理,等.某型号大推力火箭发动机试验推力测量不确定度评定[J].火箭推进,2012,38(05):81.
ZHU Zi-huan,GENG Wei-guo,GUAN Li,et al.Assessment of thrust measurement uncertainty for test of large thrust rocket engine[J].Journal of Rocket Propulsion,2012,38(01):81.
[7]宣智超,刘中祥,齐 戎.膨胀循环发动机推力室传热优化[J].火箭推进,2012,38(06):8.
XUAN Zhi-chao,LIU Zhong-xiang,QI Rong.Heat transfer optimization of thrust chamber in expansion cycle engine[J].Journal of Rocket Propulsion,2012,38(01):8.
[8]周奎,吴伟亮,张玫宝.火箭发动机喷雾均匀性数值分析[J].火箭推进,2010,36(02):26.
Zhou Kui,Wu Weiliang,Zhang Meibao.Numerical analysis on uniformity of spray in rocket engines[J].Journal of Rocket Propulsion,2010,36(01):26.
[9]张涛,唐虎,周江平,等.可贮存推进剂泵压式液体火箭发动机多次起动系统研究[J].火箭推进,2010,36(03):15.
Study on the multi-start system of turbopump-fed rocket engine with storable propellants[J].Journal of Rocket Propulsion,2010,36(01):15.
[10]刘小勇,李君,周云端.液体火箭发动机声振环境试验及统计能量分析研究[J].火箭推进,2010,36(03):49.
Liu Xiaoyong,Li Jun,Zhou Yunduan.Measurement and analysis of noise field of rocket engine based on statistical energy analysis[J].Journal of Rocket Propulsion,2010,36(01):49.
更新日期/Last Update:
1900-01-01