On-orbit Separation and Semi-Hard Landing Mechanism of Nano Moon Lander OMOTENASHI
AIAA Scitech 2020 Forum
01.01.2020
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Numerical Simulation , Propellant , CubeSat , Hard Landing , Rockets , Accelerometer , Moon , Rocket Motor , Earth , Attitude Control
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