Paper information
- Paper code
- Date
2019-10-22
- Time
12:20
- Order
12
- Room
143A
- Title
Transient process simulation of 180kN LOX/Kerosene Upper Stage Engine with RocketEngine software version 2.0
- abstract
- Session
3. Propulsion Technology (1)
- symposium
C4. IAF SPACE PROPULSION SYMPOSIUM
- congress
IAC-19
- Type of presentation
oral
Dr. Yuanqi Li, Science and Technology on Liquid Rocket Engine Laboratory, Xi’an Aerospace Propulsion Institute, China
Mr. Hongjun Liu, The 11th Institute of China Aerospace Sc. & Technology Corp., China;
Dr. Chen Hongyu, China;
Mrs. Lili Ren, National Key Laboratory of Aerospace Flight Dynamics,Northwestern Polytechnical University,Xi'an,, China;