Bell XH-15
| XR-15/XH-15 | |
|---|---|
 
 | |
| Role | Four-seat utility helicopter | 
| National origin | United States | 
| Manufacturer | Bell Helicopter | 
| First flight | 1948 | 
| Status | Canceled | 
| Primary user | United States Air Force | 
| Number built | 3 | 
The Bell XH-15 (Bell Model 54) was an American two-seat utility helicopter designed and built by Bell Helicopter, to meet a requirement for a liaison and utility helicopter for the United States Army and United States Air Force.
Development
The Model 54 was a conventional pod-and-boom four-seat helicopter with wheeled, fixed tricycle landing gear, powered by a single 275 hp Continental XO-470-5 piston engine located in the rear cabin, driving a single two-bladed rotor. The United States Army Air Forces (USAAF) ordered three in February 1946 as the XR-15. The first flight was made in March 1948 with the new designation XH-15, but no orders were forthcoming following evaluation by the United States Air Force (USAF) and the project ended in 1950.
Variants
- XR-15
 - Military designation for three Model 54s ordered for evaluation.[1]
 - XH-15
 - XR-15 redesignated before delivery.[1]
 
Operators
Specifications
Data from Bell Aircraft since 1935[2]
General characteristics
- Crew: two
 - Capacity: two passengers
 - Length: 44 ft 9 in (13.64 m) (overall length)
 - Height: 8 ft 1+1⁄2 in (2.48 m)
 - Max takeoff weight: 2,800 lb (1,270 kg)
 - Powerplant: 1 × Continental XO-470-5 piston engine, 275 hp (205 kW)
 - Main rotor diameter: 37 ft 4 in (11.38 m)
 
Performance
- Maximum speed: 105 mph (169 km/h, 91 kn)
 - Range: 200 mi (320 km, 170 nmi)
 - Service ceiling: 20,000 ft (6,100 m) (absolute ceiling)
 
See also
Related lists
References
Notes
- ^ a b Andrade 1979, p. 162
 - ^ Pelletier 1992, p. 93.
 
