Paper information

Paper code

IAC-21,C4,4,6,x65918

Date

2021-10-27

Time

12:00

Order

1006

Room

Umm Al kwain

Title

Fuel regression characteristics of axial-injection end-burning hybrid rockets using Nitrous Oxide

abstract

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Session

4. Solid and Hybrid Propulsion (2)

symposium

C4. IAF SPACE PROPULSION SYMPOSIUM

congress

IAC-21

Type of presentation

oral

Main author

Ms. Mai FUKADA, Hokkaido University, Japan

Co-authors

Mr. Hiroki Hayasaka, Hokkaido University, Japan;

Mr. Sho Suzuki, Hokkaido University, Japan;

Mr. Ayumu Tsuji, Hokkaido University, Japan;

Dr. Landon Kamps, Hokkaido University, Japan;

Dr. Masashi Wakita, Hokkaido University, Japan;

Prof. Harunori Nagata, Hokkaido University, Japan;