The Hughes XV-9, company Model 385, was a one-off American high-speed research helicopter built under a United States Army contract to prove hot-cycle propulsion. Two General Electric YT64-GE-6 turbojets served as gas generators, and their exhaust was ducted through the rotor blades to nozzles at the tips. To keep costs down it combined the side-by-side cockpit of an OH-6A with the landing gear of a Sikorsky H-34. It first flew on 5 November 1964 at Hughes's Culver City, California facility and then went to Edwards Air Force Base, where the tests were satisfactory even though the machine was noisy and burned a lot of fuel. Hughes could not solve those problems and did not develop its pressure-jet systems further. The Army tests were completed in August 1965 and the helicopter was returned to Hughes.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Hughes XV-9 (Wikipedia)
Of Make
Source Hughes XV-9 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Hughes XV-9 (Wikipedia)Lead, makerQuote, Lead, maker
was a 1960s American high-speed research helicopter built by Hughes Helicopters
Originated In
Also in Geography Atlas: where this subject originated.
Source Hughes XV-9 (Wikipedia)Operational service, testingQuote, Operational service, testing
After test flight at Hughes facility at Culver City, California
Sources
1. Hughes XV-9 (Wikipedia)
Operational service, first flight
The helicopter first flew on November 5, 1964.
Lead, maker
was a 1960s American high-speed research helicopter built by Hughes Helicopters
Design and development, propulsion
Two General Electric YT64-GE-6 turbojets were used as gas generators
Variants
United States military designation for the Hughes Model 385, one built.
Variants, units built
one built
Specifications, empty weight
Empty weight: 8,500 lb (3,864 kg)
Specifications, gross weight
Gross weight: 15,300 lb (6,955 kg)
Specifications, maximum speed
Maximum speed: 173 mph (279 km/h, 150 kn)
Operational service, testing
After test flight at Hughes facility at Culver City, California
Exemplifies: Helicopter Transport, Lead, helicopter
was a 1960s American high-speed research helicopter built by Hughes Helicopters
In Group: Vertical Takeoff and Landing Research Aircraft, Lead, type of helicopter
was a 1960s American high-speed research helicopter built by Hughes Helicopters
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