Paper information

Paper code

IAC-14,C4,5,7,x25604

Order

7

Room

714B

Title

A Linear Stability Analysis of Unique Low Frequency Mode on Uni-directional Vortex Injection Hybrid Rocket Engines

abstract

View PDF

Session

5. Propulsion Technology (2)

symposium

C4. SPACE PROPULSION SYMPOSIUM

congress

IAC-14

Type of presentation

oral

Main author

Mr. Kohei Ozawa, The University of TOKYO, Graduate school, Japan

Co-authors

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