Conceptual Design Study Based on Defined Parameters for Next-Generation Martian Rotorcrafts
2024 IEEE AEROSPACE CONFERENCE（2024）
Key words
Future Missions,Endurance Capacity,Exploration Missions,Mission Requirements,Payload Capacity,Vertical Take-off,Total Mass,Total Weight,Power Consumption,Total Power,Maximum Diameter,Figure Of Merit,Speed Of Sound,Air Density,Power Requirements,Low Reynolds Number,Disc Area,Propulsion System,Folding Mechanism,Forward Speed,Rotor Diameter,Flight Phase,Empty Weight,Lift Coefficient,Tip Speed,Electric Aircraft,Separate Planes,Large Separation,Unmanned Aerial Vehicles,Decrease In Power
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