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[2022-d-44] Theoretical and Measured Thrust Characteristics of Cold Gas Thruster Using Oxidizer of Hybrid Kick Motor

*Ryo Onodera¹, Shota Hirai¹, Landon Kamps¹, Harunori Nagata¹ (1. Hokkaido University, Department of Engineering)

キーワード：Hybrid Rocket, RCS, Cold Gas Thruster, Nitrous Oxide, Thrust Measurement