System simulation and optimal design of hybrid rocket motor with pump feed system were proposed.The high concentration hydrogen peroxide was selected as the oxidizer.Based on the fact that the high concentration hydrogen peroxide can be easily catalyzed
a pump feed system was used and a system simulation procedure was programmed.The genetic arithmetic was used in the hybrid rocket motor optimal design process.The optimal design results show that hybrid motor with a pump feed system shows more engineering application potential compared with hybrid motor with a gas pressure feed system
Cavitation modeling and start⁃up under⁃rated pressure simulation of liquid rocket engine
Numerical simulation of axial-injection end-burning hybrid rocket motor
Active control of flexible structure vibration based on fuzzy fractional order PIPID
Effect of chamber structure on fuel regression rate and performance of hybrid rocket motor
Calculation of experimental regression rate of hybrid rocket motor
Related Author
Hongyu CHEN
Yazhou LIU
Yidan CHEN
ZHANG Cheng
LIU Jun-yi
LI Yan-cheng
LU Xin
LI Xin-tian
Related Institution
National Key Laboratory of Science and Technology on Liquid Rocket Engines,Xi'an Aerospace Propulsion Institute,China Aerospace Science and Technology Corporation
China Academy of Launch Vehicle Technology, China Aerospace Science and Technology Corporation
College of Aerospace Science and Engineering, National University of Defense Technology
School of Electrical Engineering, Dalian University of Technology
School of Astronautics, Beijing University of Aeronautics and Astronautics