Grumman F-11 Tiger

· Grumman

Airplanes

Length

13.716 m

Flat Wing Span

9.4488 m

Height

3.9624 m

Flat Wing Area

23.2258 m²

Cruise Speed

927.8512 km/h

Max Speed

1168.611 km/h

Max Ceiling

14935.2 m

Number of Engines

First Flight

1954-07-30

Entry Into service

1956-01-01

Number Built

199

Maximum Take-Off Weight

10.6408 t (paragliders: kg)

Maximum Range

2055.72 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Grumman F-11 Tiger	10.6408	2055.72

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
KAI T-50 Golden Eagle	General Electric F404	13.14	9.45	Compare
Dassault Étendard IV		14.35	9.6	Compare
Hawker Hunter		13.716	10.0584	Compare
TAI Hürjet	General Electric F404	13.6	9.5	Compare
Rockwell XFV-12		13.1064	8.5344	Compare
Dassault-Breguet Super Étendard		14.31	9.6	Compare

All data (25 fields)

Name: Grumman F-11 Tiger
Manufacturer: Grumman
Description: The Grumman F11F/F-11 Tiger is a supersonic, single-seat carrier-based fighter aircraft designed and produced by the American aircraft manufacturer Grumman.
First Flight: 1954-07-30
Entry Into service: 1956-01-01
Production End: 1959-01-01
Service End: 1961-01-01
Designer: Grumman
Type: Fighter aircraft
Length (m): 13.716
Height (m): 3.9624
Cockpit Crew: 1
Max Speed (km/h): 1168.611
Cruise Speed (km/h): 927.8512
Max Ceiling (m): 14935.2
Rate of Climb (m/s): 82.804
Armament: 4 × 20 mm (.79 in) Colt Mk 12 cannon, 125 rounds per gun; 4
Number Built: 199
Powerplant Description: 1 × Wright J65-W-18 afterburning turbojet engine
Primary Users: United States Navy
Status: Retired
Wikipedia Article (URL): en.wikipedia.org/wiki/Grumman_F-11_Tiger
Flat Wing Span (m): 9.4488
Flat Wing Area (m²): 23.2258
Number of Engines: 1