Paper information

Paper code

IAC-21,C4,IP,15,x64620

Order

1015

Room

IP Area

Title

propellant mass flow rate control scheme of a deep-throttling rocket engine

abstract

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Session

IP. Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM

symposium

C4. IAF SPACE PROPULSION SYMPOSIUM

congress

IAC-21

Type of presentation

interactive

Main author

Mr. Runsheng Hu, National University of Defense Technology, China

Co-authors

Prof. Jianjun Wu, College of Aerospace Science and Engineering, National University of Defense Technology, China;

Dr. Zhenyu Chen, North China Electric Power University, China;

Dr. Yuqiang Cheng, College of Aerospace Science and Engineering, National University of Defense Technology, China;

Mr. Yu Zhang, National University of Defense Technology, China;

Mr. Honggang Liu, National University of Defense Technology, China;

Dr. Shuming Yang, National University of Defense Technology, China;