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Home Helicopter Profiles Hughes Hughes VX-9A Hot Cycle

Hughes VX-9A Hot Cycle

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General Data
First Flown:
1964
Length:
13.72 m
Lift Capability:
 
Height:
3.66 m
Range:
240 km
Rotor Span:
16.76 m
Top Speed:
222 km/h
Empty Weight:
3,856 kg
Service Ceiling:
 
Max Gross Weight:
11,567 kg
Engines:
2 General Electric YT64-GE-6 Gas turbines rated at 2,125 kW each
Armament:
n/a
Accommodations:
2 pilots Cargo: n/a
Operators:
 

     
Similar Aircraft:
none
Other Features:
Gas pressure used to drive rotors

     

     
Notes
Intended as a demonstrator for the "hot-cycle" system.
This system worked by directing the efflux of gas from the engines to cascaded canes at the tip of each blade.

Last Updated on Sunday, 31 August 2008 19:06  

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