Grumman F-11 Tiger - Specifications (F11F-1/F-11A)

Specifications (F11F-1/F-11A)

Data from Bowers 1990, p. 257.

General characteristics

• Crew: 1
• Length: 46 ft 11 in (14.3 m)
• Wingspan: 31 ft 7.5 in (9.6 m)
• Height: 13 ft 3 in (4.0 m)
• Wing area: 250 ft² (23 m²)
• Empty weight: 13,810 lb (6,277 kg)
• Loaded weight: 21,035 lb (9,561 kg)
• Max. takeoff weight: 23,459 lb (10,663 kg)
• Powerplant: 1 × Wright J65-W-18 turbojet
  • Dry thrust: 7,400 lbf (32.9 kN)
  • Thrust with afterburner: 10,500 lbf (46.7 kN)

Performance

• Maximum speed: Mach 1.1 (727 mph, 1,170 km/h) at 35,000 ft (11,000 m)
• Cruise speed: 577 mph (929 km/h)
• Range: 1,275 mi (1,110 nmi, 2,050 km)
• Service ceiling: 49,000 ft (14,900 m)
• Rate of climb: 16,300 ft/min (83 m/s)
• Wing loading: 84 lb/ft² (411 kg/m²)
• Thrust/weight: 0.50

Armament

• Guns: 4 × 20 mm (.79 in) Colt Mk 12 cannon, 125 rounds per gun
• Hardpoints: 4 with a capacity of - and provisions to carry combinations of:
  • Rockets: Aero 6A or Aero 7A "Rocket Package"
  • Missiles: AIM-9 Sidewinder
  • Other: 150 gal drop tank