Grumman F11F-1F Super Tiger

Length
14.85 m
Flat Wing Span
9.65 m
Height
4.36 m
Flat Wing Area
23.25 m²
Max Speed
2253 km/h
Max Mach
2.04 Mach
Max Ceiling
17980 m
Number of Engines
1
Aircraft Engine
First Flight
1956-05-25
Number Built
2
Maximum Take-Off Weight
11.833 t (paragliders: kg)
Maximum Range
1826 km

Pictures

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Maximum Range (km)
Grumman F11F-1F Super Tiger 11.833 1826

Similar airplanes

Name Length (m) Flat Wing Span (m)
Dassault-Breguet Super Étendard 14.31 9.6 Compare
Saab 35 Draken 15.35 9.42 Compare
Douglas F4D Skyray 13.716 10.0584 Compare
Hawker Hunter 13.716 10.0584 Compare
Dassault Étendard IV 14.35 9.6 Compare
Sukhoi Su-17 (1949) 15.253 9.6 Compare
All data (22 fields)
Name
Grumman F11F-1F Super Tiger
Manufacturer
Grumman
Description
The Grumman F11F-1F Super Tiger (company designation G-98J) is a single-seat fighter aircraft originally developed for the United States Navy (USN).
First Flight
1956-05-25
Designer
Grumman
Type
Fighter aircraft
Length (m)
14.85
Height (m)
4.36
Max Speed (km/h)
2253
Max Ceiling (m)
17980
Armament
4 × 20 mm (.79 in) Colt Mk 12 cannon, 125 rounds per gun; 4
Max Mach (Mach)
2.04
National Origin
United States of America
Number Built
2
Powerplant Description
1 × General Electric J79-GE-3A turbojet, 53.3 kN thrust each
Primary Users
United States Navy
Status
Canceled
Wikipedia Article (URL)
en.wikipedia.org/wiki/Grumman_F11F-1F_Super_Tiger
Flat Wing Span (m)
9.65
Flat Wing Area (m²)
23.25
Aircraft Engine
General Electric J79
Number of Engines
1