| Manufacturer |
Grumman |
Rockwell International |
| 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. |
The Rockwell XFV-12 was a prototype supersonic United States Navy fighter which was built in 1977. |
| First Flight |
1954-07-30 |
|
| Entry Into service |
1956-01-01 |
|
| Production End |
1959-01-01 |
|
| Service End |
1961-01-01 |
|
| Designer |
Grumman |
Rockwell International |
| Type |
Fighter aircraft |
VTOL fighter |
| Length (m) |
13.716 |
13.1064 |
| Height (m) |
3.9624 |
3.048 |
| Cockpit Crew |
1 |
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 |
1 20 mm M61 Vulcan cannon, 639 rounds; 2 AIM-7 Sparrow (carried under fuselage) and 2 AIM-9L Sidewinder AAMs or 4 AIM-7s |
| Max Mach (Mach) |
|
2.2 |
| Number Built |
199 |
1 |
| Powerplant Description |
1 × Wright J65-W-18 afterburning turbojet engine |
1 × Pratt & Whitney F401-PW-400 afterburning turbofan engine |
| Primary Users |
United States Navy |
United States Navy |
| Status |
Retired |
Cancelled (1981) |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Grumman_F-11_Tiger |
en.wikipedia.org/wiki/Rockwell_XFV-12 |
| Flat Wing Span (m) |
9.4488 |
8.5344 |
| Flat Wing Area (m²) |
23.2258 |
27.2206 |
| Number of Engines |
1 |
1 |