Directory of U.S. Military Rockets and Missiles|
Appendix 1: Early Missiles and Drones
|Copyright © 2003 Andreas Parsch|
In November 1944, Radioplane completed their model RP-14, which was evaluated by the USAAF as the OQ-6. The OQ-6 was more powerful than Radioplane's contemporary OQ-3, reaching a speed of 270 km/h (168 mph) with its 16 kW (22 hp) Righter O-45 four-cylinder engine. The model RP-15, first flown in January 1945 and most likely designated OQ-6A, had a 44 kW (60 hp) McCulloch O-90 engine, and could reach a speed of 313 km/h (195 mph).
Production orders for the OQ-6 were cancelled at the end of World War II, but a few OQ-6s remained in the USAF in 1948 for use as experimental target drones. As such they were designated XOQ-6A.
Note: Data given by several sources show slight variations. Figures given below may therefore be inaccurate!
Data for OQ-6, OQ-6A:
|Length||3 m (10 ft)|
|Wingspan||4.3 m (14 ft)|
|Weight||134 kg (295 lb)||?|
|Speed||270 km/h (168 mph)||313 km/h (195 mph)|
|Propulsion||Righter O-45 piston engine; 16 kW (22 hp)||McCulloch O-90 piston engine; 44 kW (60 hp)|
 Richard A. Botzum: "50 Years of Target Drone Aircraft", Northrop, 1985
 US Army Air Forces: "Army Aircraft Model Designations", 1946
Back to Directory of U.S. Military Rockets and Missiles, Appendix 1