Sikorsky S-67 Blackhawk

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For the utility/assault helicopter by same manufacturer, see Sikorsky UH-60 Black Hawk.
S-67 Blackhawk
Sikorsky S-67 bw lo-res.jpg
S-67 Blackhawk in 1972
Role Attack/assault helicopter
Manufacturer Sikorsky
First flight 20 August 1970
Status Destroyed (1974 crash)
Number built 1
Developed from Sikorsky SH-3 Sea King

The Sikorsky S-67 Blackhawk was a private-venture, prototype attack helicopter built in 1970 with Sikorsky Aircraft research and development (R&D) funds. A tandem, two-seat aircraft designed around the dynamic drive and rotor systems of the Sikorsky S-61, it was designed to serve as an attack helicopter or to transport up to 8 troops into combat.

Design and development

AAFSS and S-66 bid

The US Army issued a request for proposals (RFP) for its Advanced Aerial Fire Support System (AAFSS) program on 1 August 1964.[1] Lockheed offered its CL-840 design, a rigid-rotor compound helicopter.[2] Sikorsky submitted the S-66, which featured a "Rotorprop" serving as a tail rotor but as speeds increased would rotate 90° to act as pusher prop.[3] The S-66 had short, fixed wings and was powered by a Lua error in Module:Convert at line 1851: attempt to index local 'en_value' (a nil value). Lycoming T55 turboshaft engine. The design was to have a speed of Lua error in Module:Convert at line 1851: attempt to index local 'en_value' (a nil value). with the ability for Lua error in Module:Convert at line 1851: attempt to index local 'en_value' (a nil value). for brief periods.[4]

The Army awarded Lockheed and Sikorsky with contracts for further study on 19 February 1965.[1] On 3 November 1965, the Army announced Lockheed as the winner of the AAFSS program selection. The Army perceived Lockheed's design as less expensive, able to be available earlier, and that it would have less technical risk than Sikorsky's Rotorprop.[1]

S-67 development

When the Armed Aerial Fire Support System program was delayed, Sikorsky offered an armed SH-3 Sea King (Sikorsky S-61) version initially. After further AAFSS problems, the company developed an intermediate, high-speed, attack aircraft named the Sikorsky S-67 Blackhawk in 1970.[1][3][5] Design work on the S-67 began in November 1969 with manufacturing following in February 1970. The Blackhawk first flew on 20 August 1970.[6]

The S-67 featured a five-bladed main rotor and tail rotor. The main rotor was taken from the S-61, but was modified to have a hub fairing, swept main rotor blade tips and a special "alpha-1" linkage which was added to the main rotor controls to increase collective pitch sensitivity and so extend the collective pitch range. The 20° swept main rotor blade tips help to overcome a phenomenon called sub-multiple oscillating track (SMOT) that causes variations in tip track at high Mach numbers.[5][7] These allowed the S-67 to achieve and maintain high cruise speeds. To reduce drag at high speed, the main wheels retracted fully into the stub wing sponsons. It had speed brakes on the wing trailing edges[8] that could be used to decrease speed or increase maneuverability.[3]

The S-67 was fitted with a moving map display, a hands-on-collective radio tune control, and night vision systems. Its armament included a Tactical Armament Turret (TAT-140) with a Lua error in Module:Convert at line 1851: attempt to index local 'en_value' (a nil value). cannon, and could carry 16 TOW missiles, Lua error in Module:Convert at line 1851: attempt to index local 'en_value' (a nil value). rockets, or AIM-9 Sidewinder air-to-air missiles.[3] The Blackhawk was powered by two General Electric T58-GE-5 Lua error in Module:Convert at line 1851: attempt to index local 'en_value' (a nil value). engines.[9]

Operational history

Evaluation and records

The S-67 Blackhawk, along with the Bell 309 "King Cobra", was put through a series of flight test evaluations in 1972 by the U.S. Army.[10] Neither aircraft was selected to replace the AH-56 Cheyenne. Instead, the Army chose to create the new Advanced Attack Helicopter program, which would lead to the AH-64 Apache several years later.

The S-67 performed a series of aerobatic maneuvers during its various marketing tours, including rolls, split-S, and loops. The S-67 was reputed to be very smooth and responsive, in spite of its size and speed.

Piloted by Sikorsky Test Pilots Kurt Cannon and Byron Graham, the S-67 established two E-1 class world speed records on 14 December 1970 by flying at Lua error in Module:Convert at line 1851: attempt to index local 'en_value' (a nil value). over a Lua error in Module:Convert at line 1851: attempt to index local 'en_value' (a nil value). course,[11] and Lua error in Module:Convert at line 1851: attempt to index local 'en_value' (a nil value). on Lua error in Module:Convert at line 1851: attempt to index local 'en_value' (a nil value). course on 19 December 1970.[12] These records stood for 8 years.

As part of internal Sikorsky R&D efforts, in 1974 the S-67 had a Lua error in Module:Convert at line 1851: attempt to index local 'en_value' (a nil value). ducted fan fitted instead of its original conventional tail rotor.[3] The S-67 with fan was tested over 29 flight hours to compare to the conventional tail.[13] In this configuration it reached a speed of Lua error in Module:Convert at line 1851: attempt to index local 'en_value' (a nil value). in a test dive.[3] The original tail rotor and vertical tail fin were re-installed in August 1974.

Fatal crash and afterwards

The lone S-67 prototype crashed while conducting a low-level aerobatic demonstration at the Farnborough Airshow in September 1974. During a low-level roll maneuver, the nose dropped too close to the ground for safe completion of the maneuver. The aircraft struck the ground in a level attitude and immediately burst into flame. Sikorsky test pilot Stu Craig died on impact, and test pilot Kurt Cannon died nine days later from his injuries.[14] Development work on the S-67 ceased after this accident.[9]

The United States Army assigned the name Black Hawk to the Sikorsky UH-60 Black Hawk helicopter.

Specifications (S-67 Blackhawk)

Data from Illustrated Encyclopedia of Helicopters,[3] Attack Helicopter Evaluation[15]

General characteristics

  • Crew: 2
  • Capacity: Up to 15 troops[3]
  • Payload: 8,000 lb (3,600 kg)
  • Length: 74 ft 2 in (22.6 m)
  • Rotor diameter: 62 ft (18.9 m)
  • Height: 15 ft (4.57 m)
  • Airfoil: NACA 0012 Mod
  • Empty weight: 12,525 lb (5,681 kg)
  • Max. takeoff weight: 24,272 lb (11,010 kg)
  • Powerplant: 2 × T58-GE-5 turboshaft engine, 1,500 shp (1,100 kW) each
  • Rotor system: 5 blades on main rotor, 5 blades on tail rotor
  • Fuselage length: Lua error in Module:Convert at line 1851: attempt to index local 'en_value' (a nil value).
  • Fuselage height: Lua error in Module:Convert at line 1851: attempt to index local 'en_value' (a nil value).
  • Stub wing span: Lua error in Module:Convert at line 1851: attempt to index local 'en_value' (a nil value).

Performance

Armament

  • 1x 30 mm cannon, 16x TOW missiles, 70 mm rocket launchers[3]

See also

Related development
Aircraft of comparable role, configuration and era
Related lists

References

Notes
  1. ↑ 1.0 1.1 1.2 1.3 Office of the Assistant Vice Chief of Staff of the Army (OAVCSA). An Abridged History of the Army Attack Helicopter Program, pp. 4–5, 9. Washington, DC: Department of the Army. 1973.
  2. ↑ Landis and Jenkins 2000, pp. 25, 85–87.
  3. ↑ 3.0 3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 Apostolo 1984, p. 89.
  4. ↑ Landis and Jenkins 2000, p. 21.
  5. ↑ 5.0 5.1 Leoni, Ray. Black Hawk: The Story of a World Class Helicopter, p. 70. American Institute of Aeronautics and Astronautics, 2007. ISBN 978-1-56347-918-2.
  6. ↑ Yamakawa, et al. 1972, p. 1.
  7. ↑ US Patent: Blade for High Speed Helicopter
  8. ↑ Yamakawa, et al. 1972, p. 49.
  9. ↑ 9.0 9.1 Donald 1998. p. 845.
  10. ↑ Verier, Mike. Bell AH-1 Cobra, p. 138. Osprey Publishing, 1990. ISBN 0-85045-934-6.
  11. ↑ Lua error in package.lua at line 80: module 'strict' not found.
  12. ↑ Lua error in package.lua at line 80: module 'strict' not found.
  13. ↑ Cocke, Karl E. Department of the Army Historical Summary: FY 1974, Chapter XI. U.S. Army Center of Military History, 1978.
  14. ↑ Great Britain 1976.
  15. ↑ Yamakawa, et al. 1972, pp. 49–51.
Bibliography

External links

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