Paper information
- Paper code
- Order
3
- Room
Ballroom B (Crowne Plaza Hotel, -1 floor)
- Title
improvement on thrust profile flexibility by oxidizer-to-fuel ratio feedback control in hybrid rocket
- abstract
- Session
2. Propulsion System (2)
- symposium
C4. SPACE PROPULSION SYMPOSIUM
- congress
IAC-15
- Type of presentation
oral
Mr. Tomoaki Usuki, Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency, Japan
Dr. Toru Shimada, Japan Aerospace Exploration Agency (JAXA), Japan;