Hybrid Propulsion System Enabling Orbit Insertion Delta-Vs Within a 12 U Spacecraft
2019 IEEE AEROSPACE CONFERENCE（2019）
Key words
thrust vector control,attitude control,science mission phase,Jet Propulsion Laboratory,design assumptions,hybrid propulsion system,hybrid CubeSat propulsion system,hybrid motor,green propellants,propellant combination,secondary payload,gaseous oxygen,orbit insertion delta,mass 25.0 kg,time 300.0 s,velocity 800.0 m/s
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