PDF下载 分享
[1]张小平,丁丰年,刘站国,等.补燃循环发动机推进剂利用系统研究[J].火箭推进,2005,31(02):7-11.
 Zhang Xiaoping,Ding Fengnian,Liu Zhanguo,et al.Investigation of propellant utilization system for staged combustion rocket engine[J].Journal of Rocket Propulsion,2005,31(02):7-11.
点击复制

补燃循环发动机推进剂利用系统研究

相似文献/References:

[1]郑 伟,李护林,陈新红.激光快速成形技术在液体动力领域的应用前景[J].火箭推进,2015,41(06):1.
 ZHENG Wei,LI Hulin,CHEN Xinhong.Application prospect of laser rapid prototyping technology in the field of liquid power[J].Journal of Rocket Propulsion,2015,41(02):1.
[2]郭 敬,宋晶晶,孔凡超.发动机推进剂增压输送系统建模仿真技术综述[J].火箭推进,2015,41(05):1.
 GUO Jing,SONG Jingjing,KONG Fanchao.Overview of modeling and simulation technology for propellant pressurization feed system of liquid rocket engine[J].Journal of Rocket Propulsion,2015,41(02):1.
[3]于 康,谢荣华,陈晓江.表面张力贮箱电子束焊接工艺研究[J].火箭推进,2015,41(05):89.
 YU Kang,XIE Ronghua,CHEN Xiaojiang.Study on electron beam welding process for surface tension tank[J].Journal of Rocket Propulsion,2015,41(02):89.
[4]刘中华,苏 晨,汪军安,等.气路膜片设计研究[J].火箭推进,2015,41(05):95.
 LIU Zhonghua,SU Chen,WANG Junan,et al.Design and study of pneumatic diaphragm in gas circuit[J].Journal of Rocket Propulsion,2015,41(02):95.
[5]薛 薇,蔡震宇,曹红娟,等.基于可视化平台的液氢/液氧火箭发动机核心部件质量计算[J].火箭推进,2015,41(04):61.
 XUE wei,CAI Zhenyu,CAO Hongjuan,et al.Mass calculation of key assembly units in LH2/ LOX rocket engine based on visual interface[J].Journal of Rocket Propulsion,2015,41(02):61.
[6]穆朋刚,童 飞,蒲光荣,等.温度对贮箱增压系统的影响分析[J].火箭推进,2015,41(04):74.
 MU Penggang,TONG Fei,PU Guangrong,et al.Influence of temperature on tank pressurization system[J].Journal of Rocket Propulsion,2015,41(02):74.
[7]高朝辉,刘 宇,肖 肖,等.垂直着陆重复使用运载火箭对动力技术的挑战[J].火箭推进,2015,41(03):1.
 GAO Zhao-hui,LIU Yu,et al.Challenge to propulsion technology for vertical landing reusable launch vehicle[J].Journal of Rocket Propulsion,2015,41(02):1.
[8]申智帅,等.气动增压器技术及其在空间推进系统的应用[J].火箭推进,2015,41(03):15.
 SHEN Zhi-shuai,RUAN Hai-jun,et al.Pneumopump technology and its application in space propulsion system[J].Journal of Rocket Propulsion,2015,41(02):15.
[9]张 翔,徐洪平,安雪岩,等.液体火箭发动机稳态运行故障 数据聚类分析研究0[J].火箭推进,2015,41(02):118.
 ZHANG Xiang,XU Hong-ping,AN Xue-yan,et al.Clustering analysis for fault data in steady process of liquid propellant rocket engine[J].Journal of Rocket Propulsion,2015,41(02):118.
[10]窦 唯,闫宇龙,金志磊,等.某发动机涡轮泵转子高温超速/疲劳试验研究[J].火箭推进,2015,41(01):15.
 DOU Wei,YAN Yu-long,JIN Zhi-lei,et al.Fatigue experiment of turbo-pump rotor at over-speed and high temperature condition[J].Journal of Rocket Propulsion,2015,41(02):15.
[11]陈宏玉,刘红军.补燃循环发动机推力调节过程建模与仿真研究[J].火箭推进,2014,40(01):18.
 CHEN Hong-yu,LIU Hong-jun.Modeling and simulations on the thrust regulation process of staged combustion cycle rocket engine[J].Journal of Rocket Propulsion,2014,40(02):18.
[12]杨永强,刘红军,徐浩海,等.补燃循环发动机强迫起动研究[J].火箭推进,2011,37(02):14.
 YANG Yong-qiang,LIU Hong-jun,XU Hao-hai,et al.Research on forced start-up of staged combustion engine[J].Journal of Rocket Propulsion,2011,37(02):14.
[13]张小平.补燃循环发动机推力调节研究[J].火箭推进,2008,34(04):1.
 Zhang Xiaoping.lnvestlgatlon on the thrust regulation of staged combustmn cycle engine[J].Journal of Rocket Propulsion,2008,34(02):1.
[14]徐浩海,刘站国.补燃循环发动机起动过程涡轮功率控制[J].火箭推进,2006,32(04):10.
 Xu Haohai,Liu Zhanguo.Turbine power control of staged combustion cycle engine during start-up[J].Journal of Rocket Propulsion,2006,32(02):10.
[15]段小龙,刘站国,王拴虎,等.补燃循环液体火箭发动机大范围工况调节方案研究[J].火箭推进,2004,(03):1.
[16]王鹏武.全流量补燃循环液氧/甲烷发动机系统分析[J].火箭推进,2004,(06):15.
 Wang Pengwu.Analysis of FFSCC LOX/Methane Rocket Engine System[J].Journal of Rocket Propulsion,2004,(02):15.

更新日期/Last Update: 1900-01-01