Paper information
- Paper code
- Order
11
- Room
208A
- Title
Numerical Simulation of Unsteady Non-Equilibrium Flows of Hybrid Rocket Ignition using Size-Optimized Reaction Mechanism
- abstract
- Session
2. Propulsion System (2)
- symposium
C4. SPACE PROPULSION SYMPOSIUM
- congress
IAC-13
- Type of presentation
oral
Mr. Shota Yamanaka, University of Tokyo, Japan
Dr. Toru Shimada, Japan Aerospace Exploration Agency (JAXA), Japan;