Flat Wing Area
27.8709 m²
Cruise Speed
870.6551 km/h
Entry Into service
1952-12-01
Maximum Take-Off Weight
9.5254 t (paragliders: kg)
Total Fuel Capacity
2888.269
Pictures
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Total Fuel Capacity |
|
Grumman F-9 Cougar |
9.5254 |
2888.269 |
Similar airplanes
All data (27 fields)
- Name
- Grumman F-9 Cougar
- Manufacturer
- Grumman
- Description
- The Grumman F9F/F-9 Cougar is a carrier-based jet-powered fighter aircraft designed and produced by the American aircraft manufacturer Grumman.
- First Flight
- 1951-09-20
- Entry Into service
- 1952-12-01
- Service End
- 1974-01-01
- Designer
- Grumman
- Type
- Fighter aircraft
- Length (m)
- 12.192
- Height (m)
- 3.6576
- Cockpit Crew
- 1
- Max Speed (km/h)
- 1052.511
- Cruise Speed (km/h)
- 870.6551
- Min Speed (km/h)
- 205.996
- Max Ceiling (m)
- 13563.6
- Rate of Climb (m/s)
- 34.29
- Armament
- 4 × 20 mm (0.79 in) AN/M3 cannon, 190 rounds per gun; 2 × 1,000 lb (454 kg) bombs on inboard pylons plus 2 x 500 lb (227 kg) bombs on outer pylons; 6 × 5 in (127 mm) rockets
- National Origin
- United States of America
- Number Built
- 1988
- Powerplant Description
- 1 × Pratt & Whitney J48-P-8 centrifugal-flow turbojet engine
- Primary Users
- United States Navy, United States Marine Corps , Argentine Navy
- Status
- Retired
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Grumman_F-9_Cougar
- Flat Wing Span (m)
- 10.3632
- Flat Wing Area (m²)
- 27.8709
- Flat Wing Aspect Ratio
- 4
- Number of Engines
- 1