SmallSat Missions Enabled by Paired Low- Thrust Hybrid Rocket and Low-Power Long-Life Hall Thruster
2019 IEEE Aerospace Conference（2019）
关键词
mission concept analysis,outer solar system,imposed wet mass limit,mission trajectories,mission transfer times,mission activities,extra propellant mass,total wet mass limit,SmallSat missions,paired low- thrust hybrid rocket,low-power long-life Hall thruster,SmallSat-class spacecraft,combined chemical,compact hybrid rockets,high-thrust engines,thrust depending,propellant load,specific impulse,ambient vacuum environments,greater propellant throughputs,primary propulsion element,interplanetary spacecraft,recent characterization test campaign,MaSMi-DM Hall thruster,power throttling,notional low-mass spacecraft,combined hybrid rocket,low-power electric propulsion system,time 300.0 s,power 1000.0 W,time 1500.0 s,power 500.0 W,power 300.0 W,time 1940.0 s,mass 400.0 kg,time 7.5 year,time 13.5 year
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