Mikoyan-Gurevich MiG-1
| GENERAL DATA | |||
| Other Designation(s) | - |
||
| Type | Fighter and
interceptor aircraft |
Crew | 1 |
| Manufacturer(s) | Mikoyan-Gurevich |
||
| Production | 100
+ 3 prototypes (1940) |
||
| First Flight | 5 April 1940 |
Introduction | 1941 |
| Variants | |||
| Izdeliye-61 | This was the internal OKB designation of the I-200 prototype. | ||
| I-200 | MiG-1 prototype, three made. Had Mikulin AM-35 inline engine (1200 HP). | ||
| MiG-1 | Single-seat interceptor fighter aircraft for the Soviet Air Force. Production model. | ||
| DIMENSIONS | |||
| Empty Weight | 2602 kg |
Loaded Weight | 3099 kg |
| Max takeoff weight | 3319kg |
Length | 8.16 m |
| Wingspan | 10.20 m |
Wing area | 17.5 m² |
| Height | 2.62 m |
Wing Loading | 177 kg/m² |
| ARMAMENT | |||
| Main Guns | 1 x 12.7 mm Berezin UBS MG (*) |
Ammunition Carried | 300 |
| Secondary Guns | 2 × 7.62 mm ShKAS MG (**) |
Ammunition Carried | 2 x 375 |
| Other Armament | 2 ×
100 kg bombs |
||
(*, **) mounted over engine
| POWERPLANT | |||
| Engine | 1 ×
Mikulin AM-35A |
Type & Displacement | liquid-cooled V12, 46.66 L |
| Horsepower (maximum) | 1350
hp |
Power/Weight Ratio | 436 hp / ton * |
| Fuel Capacity | 2 x 110 liter
tanks
|
||
(*) with loaded weight
| PERFORMANCES | |||
| Maximum Speed | 657 km/h |
Cruise Speed | ? km/h |
| Stall Speed * | ? km/h |
Service Ceiling | 12000 m |
| Rate of Climb | 16.8 m/s |
Range | 580 km, 730 km |
(*) vitesse de décrochage
| Sources | |||
| Wikipédia | - | - |
|
Drawings |
