Flat Wing Area
33.4451 m²
Flat Wing Aspect Ratio
5.35
Cruise Speed
333.1342 km/h
Entry Into service
1959-10-01
Maximum Take-Off Weight
8.2141 t (paragliders: kg)
Total Fuel Capacity
1044.774
Maximum Range
1519.221 km
Pictures
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Total Fuel Capacity |
Maximum Range (km) |
|
Grumman OV-1 Mohawk |
8.2141 |
1044.774 |
1519.221 |
Similar airplanes
All data (31 fields)
- Name
- Grumman OV-1 Mohawk
- Manufacturer
- Grumman
- Description
- The Grumman OV-1 Mohawk is an American armed military observation and attack aircraft that was designed for battlefield surveillance, light strike and transport capabilities.
- ICAO Code
- V1
- First Flight
- 1959-04-14
- Entry Into service
- 1959-10-01
- Production End
- 1970-01-01
- Service End
- 1996-01-01
- Designer
- Grumman
- Type
- Light attack and observation aircraft
- Length (m)
- 12.4968
- Height (m)
- 3.6576
- Cockpit Crew
- 2
- Max Speed (km/h)
- 490.8499
- Cruise Speed (km/h)
- 333.1342
- Min Speed (km/h)
- 135.1849
- Max Ceiling (m)
- 7620
- Rate of Climb (m/s)
- 17.6073
- Endurance (h)
- 4.35
- National Origin
- United States of America
- Number Built
- 380
- Powerplant Description
- 2 × Lycoming T53-L-701 turboprops, 1044 kW (1400 hp) each
- Primary Users
- United States Army, Argentine Army Aviation
- Status
- Retired
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Grumman_OV-1_Mohawk
- Flat Wing Span (m)
- 14.6304
- Flat Wing Area (m²)
- 33.4451
- Flat Wing Aspect Ratio
- 5.35
- Wake Category
- M
- Aircraft Engine
- Lycoming T53
- Number of Engines
- 2