[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)

キーワード：laser fusion rocket, magnetic thrust chamber, numerical simulation