Paper information

Paper code

IAC-22,C4,IPB,16,x69962

Order

16

Room

IP Area

Title

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

abstract

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Session

IPB. Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM

symposium

C4. IAF SPACE PROPULSION SYMPOSIUM

congress

IAC-22

Type of presentation

interactive

Main author

Ms. Mai FUKADA, Hokkaido University, Japan

Co-authors

Mr. Hiroki Hayasaka, Hokkaido University, Japan;

Mr. Sho Suzuki, Hokkaido University, Japan;

Dr. Landon Kamps, Hokkaido University, Japan;

Dr. Masashi Wakita, Hokkaido University, Japan;

Prof. Harunori Nagata, Hokkaido University, Japan;