Paper information

Paper code

IAC-25,C4,4,8,x100495

Date

2025-10-01

Time

11:40

Order

8

Room

Room C4.11

Title

Performance improvement by vortex combustion for a Magnesium-Loaded HTPB/N2O Hybrid Rocket for Small Spacecraft

abstract

View PDF

Session

4. Solid and Hybrid Propulsion (2)

symposium

C4. IAF SPACE PROPULSION SYMPOSIUM

congress

IAC-25

Type of presentation

oral

Main author

Mr. Tomoya Kanda, Tokyo Metropolitan University, Japan

Co-authors

Dr. Keita Nishii, Tokyo Metropolitan University, Japan;

Prof. Akira Kakami, Tokyo Metropolitan University, Japan;