| Manufacturer |
Mikoyan-Gurevich |
Convair |
| 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 Convair Model 200 was a design for a supersonic vertical takeoff and landing (VTOL) fighter requirement for the United States Navy Sea Control Ship. |
| First Flight |
1956-01-01 |
|
| Designer |
Mikoyan-Gurevich |
Convair |
| Length (m) |
15.78 |
15.5448 |
| Height (m) |
|
5.4864 |
| Cockpit Crew |
1 |
1 |
| Max Speed (km/h) |
1960 |
|
| Max Ceiling (m) |
18800 |
|
| Armament |
2 × 30 mm Nudelman-Rikhter NR-30 autocannon |
|
| Max Mach (Mach) |
1.59 |
2 |
| National Origin |
Soviet Union |
United States of America |
| Number Built |
1 |
|
| Powerplant Description |
1 × Klimov VK-3 afterburning turbojet engine, 82.4 kN thrust each |
1 × Pratt & Whitney F401-PW-400 turbofan engine |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Mikoyan-Gurevich_I-3 |
en.wikipedia.org/wiki/Convair_Model_200 |
| Flat Wing Span (m) |
8.98 |
8.2296 |
| Flat Wing Area (m²) |
30 |
|
| Aircraft Engine |
Klimov VK-3 |
|
| Number of Engines |
1 |
1 |