AH-56 Cheyenne
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AH-56 Cheyenne | |
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AH-56 Cheyenne during testing | |
Type | Attack helicopter |
Manufacturer | Lockheed |
Maiden flight | 21 September 1967 |
Status | Canceled |
Number built | 10 |
Developed from | XH-51 |
The Lockheed AH-56A Cheyenne was a sophisticated but unsuccessful military attack helicopter. The AH-56 is a compound helicopter: the normal helicopter rotors are augmented by small wings and a propeller, giving it some of the characteristics of both helicopter and a fixed-wing aircraft.
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[edit] Development
A rigid rotor helicopter had been built by Lockheed as the XH-51 and the AH-56 followed in its path. It first flight was on 21 September 1967. The project suffered a setback on 12 March 1969 when the rotor on one prototype hit the fuselage and killed the pilot. An order for 375 had been approved in 1968 but was canceled in 1969 as a result of budget cuts, and further development was halted in 1972.
The AH-56 has a short but substantial wing on each side of the airframe and a rigid main rotor. Thrust is provided by a pusher-prop at the rear of the aircraft. Since the main rotor is not relied on for the full amount of lift (provided by the wings) or thrust (from the pusher prop), the Cheyenne is able to reach high speeds - in excess of 200 kts. The design is classed as a compound helicopter, or gyrodyne, and is unable to qualify for speed records in helicopter categories. The Cheyenne also featured an advanced navigation and fire control suite. The development of these new technologies led to many cost and time overruns. This, coupled with Vietnam war experience and an adjustment in the Army's specification[1] led to the Cheyenne's demise in favor of the AH-64 Apache, and continued production of AH-1 Cobra, which was quite successful in Vietnam, and would serve in USMC use beyond 2000. The Army would trade speed for survivability in the specification which would lead to the AH-64.
The oddest feature of the AH-56 is the gunner's station. Like the AH-1 Cobra, the AH-56 has two crew members, seated in tandem—a pilot and a gunner. A turret with a 360° firing arc is located in the middle of aircraft underbelly, in contrast to the limited forward arc of the AH-1's chin turret. The AH-56 gunner's station, seat and consoles rotate along with the turret to keep the gunner facing the same direction as the guns, although the aircraft's design obscures approximately 120° of the gunner's rear view. The gun-sight affords the gunner direct viewing from the turret. A similar, but opposite arrangement was found in the MBT-70 tank prototype: the driver sits in a counter-rotating seat in the gun turret, so that the driver always faces the front of the tank regardless of turret rotation.
[edit] Specifications
[edit] External links
- AH-56A pictures and specs
- Office of the Assistant Vice Chief of Staff of the Army (1973). "An Abridged History of the Army Attack Helicopter Program". Department of the Army (1.5MB pdf)
- Globalsecurity.org
- U.S. Centennial of Flight Commission
- TOW MISSILE SYSTEM CHRONOLOGY, Redstone Arsenal Historical Information
[edit] Related content
Related development
Comparable aircraft
Designation sequence
Related lists
- List of active military aircraft of the United States
- List of helicopters
- List of military aircraft of the United States
- List of Lockheed aircraft
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