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词条 Culver PQ-14 Cadet
释义

  1. Design and development

  2. Operational history

  3. Specifications (Culver PQ-14A)

  4. See also

  5. References

     Notes  Bibliography 

  6. External links

name=PQ-14image=Culver PQ-14B Cadet at Langley 1945.jpgcaption= Culver PQ-14B at Langley, 1945

}}{{Infobox Aircraft Type

type=Target dronemanufacturer=Culver Aircraft Companydesigner=Albert Mooneyfirst flight=introduced=1942retired=1950primary user=U.S. Army Air Corpsmore users=United States Navy
U.S. Army Air Force
United States Air Force
produced=number built= 2,043unit cost=developed from= Culver PQ-8variants with their own articles=
}}

The Culver PQ-14 Cadet is a modified version of the Culver LFA Cadet used as a target drone.

In 1940, the U.S. Army Air Corps drew up a requirement for a radio-controlled target drone for training anti-aircraft artillery gunners. The first aircraft in a series of target drones was a modification of the Culver LFA Cadet which eventually led to the PQ-14 series used throughout World War II and beyond.

Design and development

Culver proposed a modification of its civilian Model LFA Cadet which the Army purchased as the PQ-8. The success of the PQ-8 led to the development of the "NRD"; a single PQ-8 was converted to the new configuration and tested by the USAAF as the XPQ-14. Larger and faster than the PQ-8, the PQ-14 also had retractable landing gear and fuselage, wings and tail components made of wood with stressed plywood skin.

This prototype was followed by YPQ-14A service test aircraft and 1,348 PQ-14A production models. Of the latter, 1,198 were transferred to the US Navy, which designated them as TD2C-1 with the decidedly unattractive name Turkey.

The YPQ-14B was a slightly heavier variant; a total of 25 were produced before production shifted to the PQ-14B. A total of 594 PQ-14Bs served as target drones for the USAAF. A single PQ-14B was converted to use an O-300-9 engine and designated XPQ-14C. After World War II, the Culver company developed the XPQ-15 from their Model V light aircraft. After only four were delivered the company went bankrupt in 1946.

Operational history

The XPQ-14 was first flown in 1942 and began to be received in training units shortly after. The aircraft was flown unmanned, controlled by radio, but was flown by a pilot for ferry flights, utililizing a rudimentary control panel installed for that purpose and using their parachutes as a seat. Docile and easy to fly, the aircraft was finished in a bright red target color scheme although operationally, a silver or red finish was applied. Without a pilot they were flown from a "mother ship" aircraft. The typical mother ship was a Beech C-45. Despite their short lifespan, the aircraft performed well and the Franklin engine was considered "trouble-free".[1]

Most of the Culver target aircraft were "blasted out of the sky" by Army anti-aircraft gunners but a dozen or more survived and were surplused after 1950. Flown as a recreational aircraft, their new owners found that the aircraft had a sprightly performance. One is preserved as a flying example at the Planes of Fame in Chino, California,[2] another is part of the collection at the National Museum of the United States Air Force and a third N5526A, that flew to airshows throughout the 1970s holding the last airworthiness certificate[3] is displayed at the Airpower Museum at Blakesburg, Iowa.

Specifications (Culver PQ-14A)

{{aircraft specifications
|plane or copter?=plane
|jet or prop?=prop
|ref=[4]
|crew= One
|capacity=
|length main= 19 ft 6 in
|length alt= 5.94 m
|span main= 30 ft
|span alt= 9.14 m
|height main= 8 ft 4.5 in
|height alt= 2.55 m
|area main=
|area alt=
|airfoil=
|empty weight main=
|empty weight alt=
|loaded weight main= 1,830 lb
|loaded weight alt=830 kg
|useful load main=
|useful load alt=
|max takeoff weight main=
|max takeoff weight alt=
|engine (prop)= Franklin 6ACT-298-35 6-cyl. air-cooled horizontally-opposed piston engine
|number of props=1
|power main= 150 hp
|power alt= 97 kW
|power original=
|max speed main= 185 mph
|max speed alt= 300 km/h
|cruise speed main=150 mph
|cruise speed alt=241 km/h
|stall speed main=
|stall speed alt=
|never exceed speed main=
|never exceed speed alt=
|range main= 512 mi
|range alt= 823 km
|ceiling main= 17,000 ft
|ceiling alt= 5,184 m
|climb rate main=
|loading main=
|loading alt=
|thrust/weight=
|power/mass main=
|power/mass alt=
|more performance=
|armament=
|avionics=
}}

See also

{{Portal|Military of the United States|United States Air Force|Aviation}}{{aircontent
|related=
  • Culver PQ-8/Cadet

|similar aircraft=
|lists=
|see also=
}}

References

Notes

1. ^Mormillo 2001, p. 7.
2. ^Mormillo 2001, p. 7.
3. ^Air Trails, Winter 1971, p. 20.
4. ^Mormillo 2001, p. 6.

Bibliography

{{Refbegin}}
  • Mondey, David. American Aircraft of World War II (Hamlyn Concise Guide). London: Bounty Books, 2006. {{ISBN|978-0-7537-1461-4}}.
  • Mormillo, Frank B. "Defenceless Warrior: Culver's PQ-14 Drone." Air Enthusiast Issue 93, May/June 2001.
{{Refend}}

External links

{{commons category|Culver PQ-14/TD2C}}
  • Culver PQ-14/Q-14/TD2C
  • [https://web.archive.org/web/20140322014026/http://www.nationalmuseum.af.mil/factsheets/factsheet.asp?id=291 Culver PQ-14B] – National Museum of the United States Air Force
{{Culver aircraft}}{{USAF drones}}{{USAAF drones}}{{USN target drones}}

7 : Culver aircraft|United States civil utility aircraft 1940–1949|United States military utility aircraft 1940–1949|Single-engined tractor aircraft|Low-wing aircraft|Target drones of the United States|Aircraft first flown in 1942

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