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Grumman JOV-1A 'Mohawk'
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Description
  Manufacturer: | Grumman |
  Base model: | V-1 |
  Designation: | JOV-1 |
  Version: | A |
  Nickname: | Mohawk |
  Equivalent to: | AO-1A |
  Designation System: | U.S. Air Force |
  Designation Period: | 1956-Present |
  Basic role: | V/STOL |
  Modified Mission: | Observation |
  Status: | Special Test (Temporary) |
  See Also: | |
Specifications
  Length: | 41' | 12.5 m |
  Height: | 12' 8" | 3.8 m |
  Wingspan: | 42' | 12.8 m |
  Wingarea: | 330.0 sq ft | 30.6 sq m |
  Empty Weight: | 9,937 lb | 4,506 kg |
  Gross Weight: | 12,672 lb | 5,746 kg |
  Max Weight: | 15,031 lb | 6,816 kg |
Propulsion
  No. of Engines: | 2 |
  Powerplant: | Lycoming T53-L-3 |
  Horsepower (each): | 950 |
Performance
  Cruise Speed: | 207 mph | 333 km/h | 180 kt |
  Max Speed: | 308 mph | 495 km/h | 267 kt |
  Climb: | 2,950 ft/min | 899 m/min |
  Ceiling: | 30,300 ft | 9,235 m |
Examples of this type may be found at
 
Recent comments by our visitors
Cliff McKeithan barnesville, GA | The JOV-1A was developed for the U.S. Army, not the Air Force. 02/25/2001 @ 14:15 [ref: 1702] |
 
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