| Manufacturer |
Mikoyan-Gurevich |
Grumman |
| Description |
The Mikoyan-Gurevich I-3 was the first of three interrelated fighter prototype programs developed by the Mikoyan-Gurevich design bureau in the Soviet Union in the mid/late 1950s – starting with the I-3, continuing with the I-7 and finally evolving into the I-75. |
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 |
1956-01-01 |
1954-07-30 |
| Entry Into service |
|
1956-01-01 |
| Production End |
|
1959-01-01 |
| Service End |
|
1961-01-01 |
| Designer |
Mikoyan-Gurevich |
Grumman |
| Type |
|
Fighter aircraft |
| Length (m) |
15.78 |
13.716 |
| Height (m) |
|
3.9624 |
| Cockpit Crew |
1 |
1 |
| Max Speed (km/h) |
1960 |
1168.611 |
| Cruise Speed (km/h) |
|
927.8512 |
| Max Ceiling (m) |
18800 |
14935.2 |
| Rate of Climb (m/s) |
|
82.804 |
| Armament |
2 × 30 mm Nudelman-Rikhter NR-30 autocannon |
4 × 20 mm (.79 in) Colt Mk 12 cannon, 125 rounds per gun; 4 |
| Max Mach (Mach) |
1.59 |
|
| National Origin |
Soviet Union |
|
| Number Built |
1 |
199 |
| Powerplant Description |
1 × Klimov VK-3 afterburning turbojet engine, 82.4 kN thrust each |
1 × Wright J65-W-18 afterburning turbojet engine |
| Primary Users |
|
United States Navy |
| Status |
|
Retired |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Mikoyan-Gurevich_I-3 |
en.wikipedia.org/wiki/Grumman_F-11_Tiger |
| Flat Wing Span (m) |
8.98 |
9.4488 |
| Flat Wing Area (m²) |
30 |
23.2258 |
| Aircraft Engine |
Klimov VK-3 |
|
| Number of Engines |
1 |
1 |