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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
2017 -04
Start up Process Simulation of Liquid Rocket's Tank Pressure Shao Ye-tao;Luo Shu;Ran Zhen-hua;Huang Hui;Beijing Institute of Astronautical Systems Engineering;
Parameters Study of Supersonic Film Cooling of LOX/LH_2 Thrust Chamber Nozzle Zhang Zhi-hao;Xu Xiao-yong;Tian Yuan;Ding Zhao-bo;Chen Xu-yang;Beijing Aerospace Propulsion Institute;
An Optimal Control Method for Discontinuous Attitude Control System of Spacecraft Wang Yong;Li Yan-jun;Zhang Liang;Chen Yang;Tan Peng-shuo;Beijing Institute of Astronautical System Engineering;
Impact Point Control of First Sub-stage of Launch Vehicle Based on Perturbation Guidance Tang Ming-liang;Qiu Wei;Wang Ying;Zhang Xue-gong;Aerospace System Engineering Shanghai;
Experimental Research on Screw Lifting-leg with Air Cylinder Huang Fu-you;Chen Shi-chao;Huang Jie;Beijing Institute of Space Launch Technology;Inner Mongolia University of Science & Technology School of Energy & Environment;
Active Thermal Control Algorithm Based on Spacecraft Propulsion Pipeline Huang Chen;Wang Shu-wei;Yue Xiao-fei;Wang Wen-ming;Zhang Yi-chao;Beijing Institute of Astronautical Systems Engineering;
Research on Testability Analysis of Electric System in Launch Vehicle Based on Improved Multi-signal Flow Graphs Model Wang Qian-qian;Wang Hai-tao;Lan Kun;Beijing Institute of Astronautical Systems Engineering;
Motion Analysis on Structure for Space Deployment Antenna Qin Li-hua;Liu Cheng-guo;Shao Chun-shou;Duan Ya-li;Mu Li-min;Beijing Institute of Space Long March Vehicle;
Simulation on Liquid Rocket Engine Gas Infrared Characteristic Base on Finite Volume Method Wang Da-rui;Liang Wei;Ma Li-na;Yao Shi-qiang;Beijing Aerospace Propulsion Institute;
Study on Two-phase Flow Characteristics of Ignition Particles of Hydrogen Combustion System Zhao Zhong-ming;Zhao Li-qiao;Xu Xue-lei;Wang Jue;Shen Fu-dong;Beijing Institute of Space Launch Technology;China Academy of Launch Vehicle Technology;
Research on Plume Infrared Radiation of Multi-nozzle Rocket Propulsion System Qiao Ye;Nie Wan-sheng;Wu Gao-yang;Feng Song-jiang;Department of Space Equipment
Application of Adaptive Global Sliding Mode Control Method in Trajectory Tracking Wang Zi-yu;Li Jun;Wang Hai-tao;Song Jing-qun;Beijing Institute of Astronautical System Engineering;
Self-adaptive Take-off Supporting-feed-connector System Wang Ai-wei;Liu Zhong-ming;Hu Ya-tao;Wang Jian-qiu;Wang Feng-jin;Beijing Institute of Space Launch Technology;
Research and Application on MRO Technology of Space Launch Support System Based on PDM Zhang Yan;Li Mu;Yan Yong;Beijing Institute of Space Launch Technology;
Research on the Buckling Response of the Flexible Joint Based on Risks Method Huang Chao-hui;Zhang Xiao;Liu Wei-kai;The Fourth Academy of CASC;Academy of Aerospace Solid Propulsion Technology;
Research on Simulation of Launch Vehicle Pipeline Structure's Random Vibration Fatigue Lifetime Based on Finite Element Method Fang Hong-rong;Xue Li-peng;Li Zhao-hui;Beijing Institute of Astronautical Systems Engineering;
Research on Parametric Modeling and Dynamic Meshing Technology of the Hot Stage Separation of A Multi-stage Rocket Hu Xiao-jun;Wanyan Zhen-hai;Liang Lei;Li Yan;Yang Liang;Beijing Institute of Astronautical Systems Engineering;
An Optimization Design for the Force Transmission Path on the High-thrust Strap-on Launch Vehicle Mei Yong;Feng Shao-wei;The Third Engineer Scientific Research Institute of Logisric Support Department;Beijing Institute of Astronautical Systems Engineering;
Field Programmable Gate Array Hardware-Software Co-Simulation Verification Liu Hai-shan;Qiao Sen;Ding Huai-long;Beijing Research Institute of Precise Mechatronic and Controls;
Selection Method of Fault Feature Points for Missile Test Equipment Zhang Lei;Navy Submarine Academy;
Research on Gas Leakage Mechanism of Ventilated Cavitating Flows Around An Axisymmetric Body Kong De-cai;Pei Jin-liang;Yu Hai-tao;Li Yan;Beijing Institute of Astronautical Systems Engineering;
Estimation and Simulation Analysis Based on Probabilistic Model for the Effectiveness of Penetration and Defense Xie Jing-wei;Chen Wan-chun;School of Astronautics
Study on Virtual Durability Test Method of Multi-axis Heavy-duty Special Vehicle Zhang Yong-kuo;Lyu Yong-zhi;Wang Xi;Beijing Institute of Space Launch Technology;
Systematic Calibration Method Based on High-order Kalman Filter for Laser Gyro SINS Liu Bing;Ren Ji-shan;Bai Huan-xu;Wang Sheng;Chen Hong-yue;Beijing Institute of Space Launch Technology;The 8th Institute of Shanghai Academy of Spaceflight Technology;
Design of the Overall Development Process Tracking Management System Based on Workflow Technology Qiu Ya-nan;Yu Xue-song;Chen Si-jia;Beijing Institute of Astronautical Systems Engineering;
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