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Boeing Vertol YUH-61

Lighter-Than-Air Craft and Rotorcraft

The Boeing Vertol YUH-61, company Model 179, was a twin turbine-engined, medium-lift military assault and utility helicopter. It was the runner-up in the US Army Utility Tactical Transport Aircraft System competition of the early 1970s to replace the Bell UH-1 Iroquois, and Sikorsky's UH-60A won the contract at the end of the flyoff. Under a contract awarded in August 1972 Boeing Vertol designed and delivered three prototypes. Its design stressed reliability, survivability and low life-cycle cost, with dual engines, run-dry gearboxes, crashworthy armored seats and a ballistically tolerant structure, a rigid main rotor based on technology from MBB, tricycle landing gear and a pusher tail rotor. After the Army loss, its civil orders and the Navy LAMPS III hope also fell through, and a proposed attack helicopter version did not reach the Advanced Attack Helicopter downselect.

Facts
Engine Class
Turboshaft 1
Units Built
3 1
Top Speed (km/h)
286 1
Mass (kg)
4423 1
Maximum Mass (kg)
8029 1
Engine
General Electric T700 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 YUH-61 (Wikipedia)

Of Make

Boeing built this type.

Source Boeing Vertol YUH-61 (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Boeing Vertol YUH-61 (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
The Boeing Vertol YUH-61 (company designation Model 179) is a twin turbine-engined, medium-lift, military assault/utility helicopter.

Originated In

Also in Geography Atlas: where this subject originated.

Source Boeing Vertol YUH-61 (Wikipedia)Lead, country of origin
Quote, Lead, country of origin
United States Army Utility Tactical Transport Aircraft System
Sources
1. Boeing Vertol YUH-61 (Wikipedia)
  • Specifications (YUH-61A), engine name
    Powerplant: 2 × General Electric T700 turboshaft engines, 1,536 hp (1,145 kW) each
  • Specifications (YUH-61A), speed
    Maximum speed: 155 kn (178 mph, 286 km/h)
  • Specifications (YUH-61A), empty mass
    Empty weight: 9,750 lb (4,423 kg)
  • Specifications (YUH-61A), maximum takeoff
    Max takeoff weight: 17,700 lb (8,029 kg)
  • Development, units
    Three aircraft were built and a further two were cancelled and not completed.
  • Lead
    a twin turbine-engined, medium-lift, military assault/utility helicopter
  • Lead, manufacturer
    The Boeing Vertol YUH-61 (company designation Model 179) is a twin turbine-engined, medium-lift, military assault/utility helicopter.
  • Lead, country of origin
    United States Army Utility Tactical Transport Aircraft System
  • In Group: Military Transport and Utility Helicopters, Lead, role
    medium-lift, military assault/utility helicopter
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