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Missiles and Space Vehicles
FQ: 双月
AD of Publication: 北京市
Lanuage: 中文;
ISSN: 1004-7182
CN: 11-3263/V
YP: 1972
Url: 中国运载火箭技术研究院
Recommended Journals
Missiles and Space Vehicles
2014 -01
Catalog
Application of an Improved k- ε Turbulence Model for Numerical Simulation of 3-D Lateral Jet Xie Chunyan;Zhang Jingqiu;Wang Yang;Unit 63706 of PLA;
Study on Random Response Simulation and Control Ma Guoliang;Chen Liqun;Shanghai Institute of Applied Mathematics and Mechanics;Department of Mechanics, Shanghai University;
Development Tendency Analysis Based on the Research of Chinese Launch Vehicles Generation Qin Xudong;Rong Yi;Wang Xiaojun;Long Lehao;Beijing Institute of Astronautical Systems Engineering;China Academy of Launch Vehicle Technology;
Mechanical Property of the Strap-on Attachments in Launch Vehicle Feng Shaowei;Liu Zhusheng;Luan Yu;Ma Zhonghui;Yao Shidong;Beijing Institute of Aerospace Systems Engineering;China Academy of Launch Vehicle Technology;
Normalization Study on Cold-wall Heat Flux Measurement of Three Dimension Wings in Arc Wind Tunnel Xu Kao;Chen Lianzhong;Dong Yonghui;Zhang Youhua;China Academy of Aerospace and Aerodynamics;
Design Optimization and Numerical Analysis on Hydrogen Cavity of Large-Flow Thrust Chamber Ding Zhaobo;Tao Ruifeng;Sun Jiguo;Beijing Aerospace Propulsion Institute;
Four-axes Inertial Platform Simulation Technology Liu Jing;Yan Lu;Zhu Zhigang;Beijing Institute of Aerospace Control Devices;
Status and Trend of Digital Technology for Launch Vehicle Development Xiao Xiao;Li Guangzhi;Gao Zhaohui;Li Shuo;Zhang Xia;Research & Development Center, China Academy of Launch Vehicle Technology;China Academy of Launch Vehicle Technology;
Review of World Launch Vehicles in 2013 Long Xuedan;Qu Jing;Beijing Institute of Aerospace Long March Scientific and Technical Information;
Comparison Between the Numerical Simulation and Test Result for Two-Phase Flow in the Internal Cavity of Cavitating Venturi Zhu Ziyong;Liu Hongtong;Sun Wanmin;Beijing Institute of Aerospace Testing Technology;
Research on Missile Separation Design Techniques Guo Fengmei;Yu Menglun;Sichuan Academy of Aerospce Technology;Beijing Institute of Aerospace Systems Engineering;
Review of World Ballistic Missiles in 2013 Liu Chang;Yang Yunxiang;Xia Wei;Zhang Ying;Beijing Institute of Aerospace Long March Scientific and Technical Information;
Feasibility Research on Perpendicular Reentry of Kinetic Energy Payload Feng Biming;Nie Wansheng;Li Ke;Academic of Equipment;
An Initial Alignment Algorithm for the Redundant Strapdown Inertial Navigation System in the Missile Wang Yuegang;Yang Jiasheng;Wen Chaobin;Yang Bo;Department of Automatic Control Engineering, The Second Artillery Engineering University;Unit 96363 of PLA;
A Multi-level Collaboration Low-power Design Based on OR1200 Zhang Yi;Wang Xiang;Lu Ying;Zhao Zexi;School of Electrical Engineering, Beihang University;
Calibration of Strapdown Inertial Navigation System/Odometer Integrated Navigation System Based on Recursive Least Square Method Luo Qiangli;Han Junhai;Beijing Institute of Aerospace Control Device;
Attitude Measurement for Relative Object Based on Binocular Vision Kang Xinuo;Yao Dongxing;China Airborne Missile Academy;Beijing Romtek Developing Co.,LTD;
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