North American MQM-42 Redhead-Roadrunner
| MQM-42 Redhead | |
|---|---|
| 
 
 MQM-42A  | |
| Type | Target drone | 
| Place of origin | United States | 
| Service history | |
| In service | 1961 - mid-1970s[1] | 
| Used by | United States Army | 
| Production history | |
| Manufacturer | North American Aviation | 
| Specifications | |
| Weight | 400 kilograms (880 lb) | 
| Length | 7.57 metres (24.8 ft) | 
| Diameter | 30 centimetres (12 in) | 
| 
 | |
| Wingspan | 1.90 metres (6 ft 3 in) | 
| Propellant | 
 solid-fuel booster  | 
Operational range  | 400 kilometres (250 mi) | 
| Flight ceiling | 18,000 metres (59,000 ft) | 
| Speed | Between Mach .09 and Mach 2+ | 
The MQM-42 Redhead was an American high altitude supersonic drone manufactured by North American Aviation (as model NA-273 Redhead/Roadrunner) used by the U.S. Army for testing and training as a high-performance target for the MIM-23 Hawk air-defense missile system.
The Redhead variant was used for high-altitude testing and the Roadrunner for low altitude. The MQM-42 was launched by a Rocketdyne solid-propellant RATO booster, derived from the solid fuel motor for the U.S. Army's Little John battlefield rocket, and was recovered by parachute. NAA manufactured the NA-273 in Columbus, Ohio. The sustainer engine was a Marquardt MA-74 ramjet.
In June 1963, it was designated as MQM-42A.
References
| Wikimedia Commons has media related to North American Aviation. | 
- ↑ "North American MQM-42 Redhead/Roadrunner". Directory of U.S. Military Rockets and Missiles.
 
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