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Kellett KD 1

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Top speed
  
201 km/h

First flight
  
1934

Length
  
8.79 m


Manufacturer
  
Kellett Autogiro Corporation

Mini r c autogyro inspired by the kellett kd 1 flying outdoor


The Kellett KD-1 was a 1930s American autogyro built by the Kellett Autogiro Company. It had the distinction of being the first practical rotary-wing aircraft used by the United States Army and inaugurated the first scheduled air-mail service using a rotary-wing aircraft.

Contents

Kellett KD-1 httpsuploadwikimediaorgwikipediacommonsthu

Development

Kellett KD-1 Kellett KD1 helicopter development history photos technical data

Using the experience gained in building Cierva autogyros under licence the Kellett Autogiro Company developed the KD-1 which was similar to the contemporary Cierva C.30. It had two open cockpits, a fixed tailwheel landing gear and was powered by a 225 hp (168 kW) Jacobs L-4 radial engine. After testing of the prototype a commercial variant designated the KD-1A was put into production. The KD-1A had a three-bladed rotor with folding blades and a number of minor detail improvements. A KD-1B which was a KD-1A with an enclosed cockpit for the pilot was operated by Eastern Airlines and inaugurated the first scheduled rotary-wing air-mail service on 6 July 1939.

Kellett KD-1 Kellett KD1 helicopter development history photos technical data

In 1935 the United States Army bought a KD-1 for evaluation and designated it the YG-1, a second aircraft followed which had additional radio equipment and was designated the YG-1A. These two aircraft were followed by a batch of seven designated YG-1B. In 1942 seven more were bought for use in the observation role as the XO-60. Six XO-60s were re-engined with 300 hp (224 kW) Jacobs R-915-3s and re-designated YO-60. One YG-1B was modified with a constant-speed rotor and was re-designated the YG-1C, it was later re-engined with the more powerful R-915 and re-designated again as the XR-2. The XR-2 was destroyed by rotor ground resonance problems and the evaluation was continued with another modified YG-1B designated the XR-3.

Variants

Kellett KD-1 Kellett
KD-1
Prototype, one built
KD-1A
Commercial variant with open cockpit and a 225 hp (168 kW) Jacobs L-4 radial engine; three built.
KD-1B
Commercial variant with enclosed cockpit; two built.
YG-1
United States Army designation for one KD-1A acquired for evaluation.
YG-1A
One aircraft as YG-1 with the addition of radio equipment.
Kellett KD-1 Kellett
YG-1B
Production aircraft for the United States Army; seven built.
YG-1C
One YG-1B modified with a constant-speed rotor for evaluation, later designated the XR-2.
Kellett KD-1 Kellett KD1 helicopter development history photos technical data
XO-60
Production aircraft for the United States Army with a 225 hp (168 kW) Jacobs R-755 radial engine, seven built.
YO-60
Six XO-60s re-engined with a 300 hp (220 kW) Jacob R-915-3 radial engine.
XR-2
The YG-1C re-designated after being re-engined with a 300 hp (220 kW) Jacobs R-915-3 radial engine.
XR-3
One YG-1B modified to XR-2 standard for evaluation.
Kayaba Ka-Go prototype
Prototype, based on a KD-1A airframe repaired by Kayaba.
Kayaba Ka-1
Imperial Japanese Army development of the Ka-Go, powered by a 240 hp (180 kW) Argus As 10 engine.
Kayaba Ka-2
Imperial Japanese Army development of the Ka-1, powered by a 245 hp (183 kW) Jacobs L-4MA-7 engine.

Operators

 United States
  • Eastern Airlines
  • United States Army Air Forces
  • Specifications (KD-1B)

    General characteristics

  • Crew: 2
  • Length: 28 ft 10 in (8.79 m)
  • Performance

    References

    Kellett KD-1 Wikipedia