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Grumman F11F-1F Super Tiger

Supersonic and Experimental Aircraft

The Grumman F11F-1F Super Tiger, company designation G-98J, was a single-seat fighter developed for the United States Navy from the F11F-1 Tiger. It came from a 1955 study of fitting the new General Electric J79 engine into the Tiger airframe, and the Navy authorized the modification of two production F11F-1s with enlarged air intakes and YJ79 turbojets. The first flight was on 25 May 1956, and after wing root fillets, a short fuselage extension and an uprated engine the aircraft reached Mach 2.04 in 1957, the first naval aircraft to exceed Mach 2. It also set a world altitude record in 1958. The Navy never ordered it into production, and Grumman failed to sell it to Switzerland, Germany, Japan or Canada, who chose other aircraft.

Facts
Year
1956 1
Engine Class
Jet 1
Status
Cancelled 1
Units Built
2 1
Top Speed (km/h)
2253 1
Mass (kg)
6264.1 1
Maximum Mass (kg)
11,832 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Grumman F11F-1F Super Tiger (Wikipedia)

Of Make

Source Grumman F11F-1F Super Tiger (Wikipedia)
Sources
1. Grumman F11F-1F Super Tiger (Wikipedia)
  • Lead sentence, country
    The Grumman F11F-1F Super Tiger (company designation G-98J) is a single-seat fighter aircraft originally developed for the United States Navy (USN).
  • Design and development, first flight
    The aircraft first flew on 25 May 1956, reaching Mach 1.44 in one of the flights.
  • Design and development, no production order
    However, the U.S. Navy did not order the Super Tiger into production.
  • Lead, prototypes only
    the F11F-1F did not proceed beyond the two F11F-1F prototypes.
  • Specifications (F11F-1F), powerplant
    Powerplant: 1 × General Electric J79-GE-3A turbojet, 12,533 lbf (55.75 kN) thrust dry, 17,000 lbf (76 kN) with afterburner
  • Specifications (F11F-1F), maximum speed
    Maximum speed: 1,400 mph (2,253 km/h, 1,200 kn) at 40,000 ft (12,200 m)
  • Specifications (F11F-1F), empty weight
    Empty weight: 13,810 lb (6,277 kg)
  • Specifications (F11F-1F), maximum takeoff weight
    Max takeoff weight: 26,086 lb (11,833 kg)
  • Of Make: Grumman, Lead sentence
    The Grumman F11F-1F Super Tiger (company designation G-98J) is a single-seat fighter aircraft originally developed for the United States Navy (USN).
  • In Group: High-Speed Military Prototypes and Reconnaissance Aircraft, Lead sentence
    The Grumman F11F-1F Super Tiger (company designation G-98J) is a single-seat fighter aircraft originally developed for the United States Navy (USN).
  • Exemplifies: Aviation, Lead sentence
    The Grumman F11F-1F Super Tiger (company designation G-98J) is a single-seat fighter aircraft originally developed for the United States Navy (USN).
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