Sikorsky XH-39

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Sikorsky S-59
Type Helicopter
Manufacturer Sikorsky Aircraft Corporation
Introduced not produced
Number built one[1]
Variants H-18

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).

Contents

[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

[edit] Notes

  1. ^ Polmar, Norman, and Kennedy, Floyd D., Jr. Military Helicopters of the World (Annapolis, MD: Naval Institute Press, 1981), p.288.
  2. ^ Polmar and Kennedy, p.288.
  3. ^ Polmar and Kennedy, p.288.
  4. ^ Harding 1990, p.233.

[edit] Bibliography