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Kellett KD-1
Kellett XR-3 modification of YG-1B (KD-1) of U.S. Army preserved at Yanks Air Museum, Chino airfield California, in January 2008
Role Autogyro
National origin United States
Manufacturer Kellett Autogiro Company
First flight 1934
Primary users United States Army Air Force
Eastern Airlines

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

Development

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 225hp (168kW) 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.

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 300hp (224kW) 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

KD-1
Prototype, one built
KD-1A
Commercial variant with open cockpit and a 225hp (168kW) 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.
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.
XO-60
Production aircraft for the United States Army with a 225hp (168kW) Jacobs R-755 radial engine, seven built.
YO-60
Six XO-60s re-engined with a 300hp (224kW) Jacob R-915-3 radial engine.
XR-2
The YG-1C re-designated after being re-engined with a 300hp (224kW) Jacobs R-915-3 radial engine.
XR-3
One YG-1B modifed to XR-2 standard for evaluation.
Kayaba Ka-Go Prototype
Prototype, It was an airframe which had repaired KD-1A by Kayaba.
Kayaba Ka-1
Imperial Japanese Army developed referring to KD-1A. Powered by a 240hp (179kW) Argus As 10 engine, Airframe that changed engine of prototype.
Kayaba Ka-2
Imperial Japanese Army developed referring to KD-1A. Powered by a 245 hp (183 kW) Jacobs L-4MA-7 engine, Airframe that changed engine of Ka-1 for the same thing as prototype.

Operators

 Japan
 United States

Specifications (KD-1B)

General characteristics

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

Performance

See also

Comparable aircraft

Related lists

References

  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.  
  • The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.  
  • Andrade, John (1979). U.S.Military Aircraft Designations and Serials since 1909. Midland Counties Publications. ISBN ISBN 0 904597 22 9.  
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