Paper information

Paper code

IAC-12,C4,2,26.p1,x15923

Order

26

Room

TS14 (Sala Capri, Palacongressi)

Title

Performance advancement of hybrid rocket engine through higher regression rate and combustion efficiency with multi-section swirl injection method

abstract

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Session

2. Propulsion System (2)

symposium

C4. SPACE PROPULSION SYMPOSIUM

congress

IAC-12

Type of presentation

poster

Main author

Mr. Yoshihide Hirata, Kyushu University, Japan

Co-authors

Mr. Sho Ohyama, Kyushu University, Japan;

Prof. Shigeru Aso, Kyushu University, Japan;

Dr. Yasuhiro Tani, Kyushu University, Japan;

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