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Boeing Vertol XCH-62

Lighter-Than-Air Craft and Rotorcraft

The Boeing Vertol XCH-62, Model 301, was a triple-turbine heavy-lift helicopter project designed for the United States Army by Boeing Vertol. Approved in 1971, one prototype reached 95 percent completion before the programme was cancelled in 1975, and that prototype was scrapped in 2005. It grew from a Heavy Lift Helicopter request issued in November 1970 and was a tandem-rotor design with four blades on each 92 ft rotor, a high-mounted fuselage and widely spaced landing gear that would let it straddle cargo, and it was meant to lift a standard 20-foot MILVAN container weighing up to 22.4 short tons. Three Allison XT701-AD-700 turboshafts powered it, and it was designed as the first helicopter with fly-by-wire flight controls and no mechanical backup. It was the largest helicopter ever built in the western countries.

Facts
Engine Class
Turboshaft 1
Status
Scrapped 1
Units Built
1 1
Top Speed (km/h)
269 1
Mass (kg)
27,025 1
Engine
Allison XT701-AD-700 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes

An aircraft, so it exemplifies the aviation mode.

Source Boeing Vertol XCH-62 (Wikipedia)

Of Make

Boeing built this type.

Source Boeing Vertol XCH-62 (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Boeing Vertol XCH-62 (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
The Boeing Vertol XCH-62 (Model 301) was a triple-turbine, heavy-lift helicopter project designed for the United States Army by Boeing Vertol.

Originated In

Also in Geography Atlas: where this subject originated.

Source Boeing Vertol XCH-62 (Wikipedia)Lead, country of origin
Quote, Lead, country of origin
designed for the United States Army by Boeing Vertol
Sources
1. Boeing Vertol XCH-62 (Wikipedia)
  • Lead, fate
    The prototype was scrapped in 2005.
  • Design, engines
    The helicopter was powered by three Allison XT701-AD-700 turboshafts
  • Design, engine name
    The helicopter was powered by three Allison XT701-AD-700 turboshafts
  • Specifications (XCH-62A), empty mass
    Empty weight: 59,580 lb (27,025 kg)
  • Specifications (XCH-62A), speed
    Maximum speed: 145 kn (167 mph, 269 km/h) with external load
  • Lead, units
    one prototype reached 95% completion before it was canceled in 1975
  • Lead
    a triple-turbine, heavy-lift helicopter project
  • Lead, manufacturer
    The Boeing Vertol XCH-62 (Model 301) was a triple-turbine, heavy-lift helicopter project designed for the United States Army by Boeing Vertol.
  • Lead, country of origin
    designed for the United States Army by Boeing Vertol
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