Overview
The Grumman F9F-6 Cougar was developed as a swept-wing derivative of the F9F Panther. Introduced in the early 1950s, it improved performance in the transonic regime. The aircraft served with the U.S. Navy and Marine Corps.
Live Fleet Activity (F9F6)
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Specifications
Units
- Engine
- 1 × Pratt & Whitney J48-P-8
- Engine type
- Jet
- Thrust
- 7,250 lbf · 32 kN
- Avionics
- AN/APG-30, AN/ARC-27, AN/APN-1 etc.
- Wing tips
- No winglets
- Seats
- 1
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- 40 ft 11 in · 12.47 m
- Tail height
- 12 ft 4 in · 3.75 m
- Fuselage diameter
- 4 ft 11 in · 1.50 m
- Wing span
- 34 ft 6 in · 10.52 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 21,000 lb · 9,550 kg
- Max landing weight
- 15,800 lb · 7,150 kg
- Max payload
- 3,100 lb · 1,400 kg
- Fuel capacity
- 920 gal · 3,500 L · 2,800 kg (Jet A)
- Max cruise speed
- 568 kt · 654 mph · 1,052 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 93 kt · 107 mph · 172 km/h
- Range
- 915 nm · 1,050 mi · 1,690 km
- Fuel burn
- —
- Ceiling
- 44,500 ft · 13,600 m
- Rate of climb
- 6,750 ft/min · 34 m/s
- Takeoff distance
- 2,100 ft · 640 m
- Landing distance
- 1,360 ft · 420 m
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Live fleet activity details
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