Engineering:Culver PQ-10
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PQ-10 | |
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Role | Target drone |
National origin | Culver Aircraft Company |
Primary user | United States Army Air Forces |
Number built | 0 |
Developed from | Culver Model MR |
The Culver PQ-10 was an American target drone, designed by the Culver Aircraft Company for use by the United States Army Air Forces . Designed in 1941, the project was cancelled before any aircraft flew.
Design and development
The prototype XPQ-10 was ordered by the United States Army Air Forces in 1941. Derived from the civilian Culver Model MR, the XPQ-10 was a high-wing monoplane equipped with twin Franklin O-300 engines and a fixed tricycle landing gear.[1] Plans were made for the production of PQ-10 series aircraft; however, before the XPQ-10 was completed, the project was cancelled.[2]
Specifications (XPQ-10)
Data from Parsch[1]
General characteristics
- Crew: 1 (Optional)
- Length: 16 ft 7 in (5.05 m)
- Wingspan: 30 ft (9.1 m)
- Height: 4 ft 6 in (1.37 m)
- Powerplant: 2 × Franklin O-300 opposed piston engines, 175 hp (130 kW) each
See also
Aircraft of comparable role, configuration and era
Related lists
References
- Citations
- Bibliography
- Juptner, Joseph P. U.S. Civil Aircraft Series, Volume 8. New York: McGraw-Hill Professional, 1993. ISBN:978-0830643738.
- Parsch, Andreas (2009). "PQ Series". Directory of U.S. Military Rockets and Missiles Appendix 1: Early Missiles and Drones. designation-systems.net. http://www.designation-systems.net/dusrm/app1/pq#_PQ10.html. Retrieved 2011-02-16.
![]() | Original source: https://en.wikipedia.org/wiki/Culver PQ-10.
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