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Hoverbike
The Hoverbike is a Wingless eVTOL aircraft developed by Malloy Aeronautics in Boston, United States. It is currently in the Manned Flight Testing phase. Its first manned flight test was carried out in June 2015. The Hoverbike aircraft has a capacity of one (1) occupant. For more information on this aircraft, see their website.
Last updated on February 26th, 2024.
Characteristics
General | |
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Name | Hoverbike |
Company | Malloy Aeronautics |
Industry | Start-ups |
City | Boston |
Country | United States |
Primary Classification | Wingless |
Secondary Classification | |
Tertiary Classification | Personal Flying Device |
Energy Source | Battery |
Capacity | 1 seat |
Pilot type | Piloted |
Announced | June 2015 |
First (Unmanned) Flight | |
First (Manned) Flight | 2015-06-22 |
Design Maturity | Manned Flight Testing |
Official Website | https://www.hover-bike.com/ |
Geometry | |
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Length | |
Height | |
Span | |
Wing Configuration | |
Wing sweep? |
Seating | |
---|---|
|
|
Seating Configuration | 1 seat |
Passenger Seat Rows | |
Seats per Row | |
Separated pilot seat? | Yes |
Seating Layout | Standard |
Performance | |
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Max Take-off Weight (MTOW) | |
Operating Empty Weight (OEW) | |
Payload | 130 kg |
Battery Mass | |
Cruise Speed | |
Max Speed | |
Range | |
Endurance | |
Cruise Altitude | |
Max Altitude | |
Thrust | |
Power Available |
Propulsors | |
---|---|
Propulsor Type | Fan |
Propulsor Layout | |
Total Number of Propulsors | 4 |
Propulsors in Cruise | |
Propulsor in Hover | 4 |
Individual Propulsor Thrust | |
Individual Propulsor Power |
Electric Energy | |
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Battery Capacity | |
Battery Power | |
Battery Density | |
Battery Current | 0.00 |
Battery Voltage | |
Battery Chemical System | |
Battery Charge Time | |
Battery Charge Rate | |
Charging Voltage |
Maneuverability | |
---|---|
Wheeled Ground Taxi? | No |
Independent Ground Taxi? | |
Conventional Landing? | |
Amphibious? |