Paper information

Paper code

IAC-15,C4,2,5,x29524

Order

5

Room

Ballroom B (Crowne Plaza Hotel, -1 floor)

Title

Performance Calculations and Burning Tests on Altering-intensity Swirling Oxidizer Flow Type Hybrid Rocket Engines

abstract

View PDF

Session

2. Propulsion System (2)

symposium

C4. SPACE PROPULSION SYMPOSIUM

congress

IAC-15

Type of presentation

oral

Main author

Mr. Kohei Ozawa, Japan Aerospace Exploration Agency (JAXA), ISAS, Japan

Co-authors

Dr. Koki Kitagawa, Japan Aerospace Exploration Agency (JAXA), ISAS, Japan;

Dr. Toru Shimada, Japan Aerospace Exploration Agency (JAXA), Japan;