Hybrid Propulsion Mars Ascent Vehicle Concept Flight Performance Analysis
2017 IEEE AEROSPACE CONFERENCE（2017）
Key words
hybrid propulsion Mars ascent vehicle concept,flight performance analysis,high-fidelity simulation,end-to-end performance evaluation,dynamics simulator for entry, descent and surface landing,DSENDS,multibody component modelling,Martian environment,flight software,mission timeline,end-to-end MAV flight performance
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