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VC200
The VC200 is a Wingless eVTOL aircraft developed by Volocopter in Mannheim, Germany. It is currently in the Scaled Prototype phase. Its first manned flight test was carried out in March 2016. The VC200 aircraft has a capacity of one (1) occupant. It also has a cruise speed of 102 units, For more information on this aircraft, see their website.
Last updated on February 26th, 2024.
Characteristics
General | |
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Name | VC200 |
Company | Volocopter |
Industry | Minor aerospace |
City | Mannheim |
Country | Germany |
Primary Classification | Wingless |
Secondary Classification | |
Tertiary Classification | Multicopter |
Energy Source | Battery |
Capacity | 1 seat |
Pilot type | Piloted |
Announced | November 2013 |
First (Unmanned) Flight | |
First (Manned) Flight | 2016-03-30 |
Design Maturity | Scaled Prototype |
Official Website | http://www.volocopter.com/ |
Geometry | |
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Length | 9.2 m |
Height | 2 m |
Span | 9.2 m |
Wing Configuration | |
Wing sweep? |
Seating | |
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|
|
Seating Configuration | 1x1 |
Passenger Seat Rows | 1 seat |
Seats per Row | 1 seat |
Separated pilot seat? | |
Seating Layout | Standard |
Performance | |
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Max Take-off Weight (MTOW) | 450 kg |
Operating Empty Weight (OEW) | 300 kg |
Payload | 150 kg |
Battery Mass | |
Cruise Speed | 55 kt |
Max Speed | |
Range | |
Endurance | |
Cruise Altitude | |
Max Altitude | 6500 m |
Thrust | |
Power Available |
Propulsors | |
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Propulsor Type | Prop |
Propulsor Layout | |
Total Number of Propulsors | 18 |
Propulsors in Cruise | |
Propulsor in Hover | 18 |
Individual Propulsor Thrust | |
Individual Propulsor Power | 3.9 kW |
Electric Energy | |
---|---|
Battery Capacity | |
Battery Power | |
Battery Density | |
Battery Current | |
Battery Voltage | |
Battery Chemical System | Lithium-ion |
Battery Charge Time | 120 min |
Battery Charge Rate | |
Charging Voltage |
Maneuverability | |
---|---|
Wheeled Ground Taxi? | No |
Independent Ground Taxi? | |
Conventional Landing? | |
Amphibious? |