Overview
The Bell V-280 Valor is a tiltrotor aircraft and a joint development of Bell Helicopter and Lockheed Martin under the Future Vertical Lift (FVL) program of the United States Army. The Valor is designed to provide the perfect value in terms of cost, performance, operations, and structure, with its reliability and improved systems.
Specifications
Units
- Engine
- 2 × General Electric T64
- Engine type
- Turboshaft
- Power
- 2 × 5,000 shp · 3,729 kW
- Avionics
- Moog Inc. Flight Control System
- Wing tips
- No winglets
- Seats
- 14
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- 50 ft 6 in · 15.40 m
- Tail height
- 23 ft 0 in · 7.00 m
- Fuselage diameter
- —
- Wing span
- 35 ft 1 in · 10.70 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 57,500 lb · 26,000 kg
- Max landing weight
- —
- Max payload
- 12,000 lb · 5,450 kg
- Fuel capacity
- Max cruise speed
- 300 kt · 345 mph · 556 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 800 nm · 920 mi · 1,480 km
- Fuel burn
- —
- Ceiling
- 25,000 ft · 7,600 m
- Rate of climb
- 4,500 ft/min · 23 m/s
- Takeoff distance
- —
- Landing distance
- —
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