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The Sikorsky XH-39 (manufacturer designation S-59), developed by Sikorsky Aircraft Corporation in 1954, was the U.S. Army’s first turbine-powered helicopter. It was fast and innovative, but ultimately rejected by the U.S. Army, in favor of the Bell UH-1.
It was a four seat helicopter that used a 400hp (298 kW) XT51-T-3 (Artouse II) turbine engine. It was developed from the previous Sikorsky model, the H-18 (company model S-52), and had the same layout. It differed in using retractable tricycle landing gear,[2] modified tail rotor, and four-blade main rotor.[3]
On August 26, 1954, the S-59 set a world helicopter speed record of 155.9 mph (251 km/h). The same year, it set a world helicopter altitude record of 24500 ft (7474 m).
[edit] Specifications (H-39)
Data from U.S. Army Aircraft Since 1947 [4]
General characteristics
- Crew: Four
- Length: 41 ft 0 in (12.50 m)
- Rotor diameter: 35 ft 0 in (10.67 m)
- Height: 9 ft 7 in (2.92 m)
- Disc area: 962 ft² (89.4 m²)
- Empty weight: 2,105 lb (957 kg)
- Loaded weight: 3,361 lb (1,528 kg)
- Powerplant: × Turbomeca XT51-T-3 Artouste turboshaft, 400 shp (298 kW) each
Performance
[edit] References
- ^ Polmar, Norman, and Kennedy, Floyd D., Jr. Military Helicopters of the World (Annapolis, MD: Naval Institute Press, 1981), p.288.
- ^ Polmar and Kennedy, p.288.
- ^ Polmar and Kennedy, p.288.
- ^ Harding 1990, p.233.
[edit] Bibliography
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