Overview
2014–Onward
$4.5 million
The Sikorsky X2 Technology demonstrator was developed to explore high-speed compound helicopter flight. It aimed to significantly exceed traditional helicopter cruise speeds while retaining vertical takeoff capability. The aircraft validated several advanced rotorcraft concepts.
Specifications
Units
- Engine
- 1 × LHTEC T800-LHT-801 turboshaft
- Engine type
- Turboshaft
- Power
- 1,800 shp · 1,342 kW
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 2
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- —
- Tail height
- —
- Fuselage diameter
- —
- Wing span
- —
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 7,950 lb · 3,600 kg
- Max landing weight
- —
- Max payload
- —
- Fuel capacity
- 80 gal · 300 L · 200 kg (Jet A)
- Max cruise speed
- 248 kt · 285 mph · 459 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 702 nm · 810 mi · 1,300 km
- Fuel burn
- 9.36 nm/gal · 4.58 km/L
- Ceiling
- —
- Rate of climb
- —
- Takeoff distance
- —
- Landing distance
- —
Gallery
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