[B-10] Fusion Rocket / Magneto Plasma Sail

[2022-b-40] Quantitative evaluation of the impulse-bit generated in a magnetic thrust chamber

*Taiki Inatomi¹, Taichi Morita², Naoji Yamamoto², Hideki Nakashima², Tomihiko Kojima¹, Eisuke Kuramoto¹, Masaki Ikebe¹, Atsushi Sunahara³, Shinichi Namba⁴, Toshiyuki Ise⁵, Kazuhiro Yagi⁵, Yoshitaka Mori⁶, Tomoyuki Johzaki⁴ (1. Kyushu University Interdisciplinary graduate school of Engineering Sciences, 2. Kyushu University Faculty of Engineering Sciences, 3. Purdue University department of nuclear engineering , 4. Hiroshima University department of advanced science and engineering, 5. IHI Aerospace Co., Ltd., 6. The Graduate School for the Creation of New Photonics Industries)

Keywords:laser fusion rocket, magnetic thrust chamber, numerical simulation