Mikoyan-Gurevich MiG-5T
| GENERAL DATA | |||
| Other Designation(s) | DIS |
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| Type | Heavy Fighter, Escort Fighter |
Crew | 1 |
| Manufacturer(s) | Mikoyan-Gurevich OKB |
||
| Production | 2 |
||
| First Flight | 11 June 1941 |
Status | Cancelled |
| Variants | |||
| DIS | basic designation | ||
| DIS-T | initial prototype with 2 × Mikulin AM-37 inline engines with 1400 hp each. | ||
| DIS-IT | second prototype with 2 × Shvetsov M-82F radial engines with 1,700 hp each; other subtle revisions added to improved performance. | ||
| MiG-5 | reserved Soviet Air Forces designation for production-quality aircraft (not used). | ||
| DIMENSIONS | |||
| Length | 11.20 m |
Empty Weight | 6140 kg |
| Wingspan | 15.3 m |
Loaded Weight | 8060 kg |
| Height | 3.40 m |
Max takeoff weight | ? kg |
| Wing area | 38.9 m² |
Wing Loading | 207.2 kg/m² |
| ARMAMENT | |||
| Main Guns | 23 mm Volkov-Yartsev VYa-23 * |
Ammunition Carried | 200 |
| Secondary Guns | 2 × 12.7 mm Berezin UB MG ** | Ammunition Carried | 2 x 300 |
4 × 7.62 mm ShKAS MG *** |
4 x 1000 |
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| Other Armament | until 1000 kg of bombs or 1 torpedo (gun pod removed) |
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(*) in a pod beneath the nose, (**) wing roots (synchronized), (***) wing roost (synchronized)
Modified: 2 x 23mm VYa cannon in removable ventral gun pof, 4 x 7.62 mm ShKAS MG in wing roots
| POWERPLANT | |||
| Engine | 2 × Mikulin AM-37 |
Type & Displacement | V-12 liquid-cooled, 45.84 L |
| Horsepower (maximum) | 2 x 1400
hp |
Power/Weight Ratio | 347.39 hp / ton * |
| Fuel Capacity | 1920 L (inside)
|
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(*) with loaded weight
| PERFORMANCES | |||
| Maximum Speed | 610 km/h at 6800 m |
Cruise Speed | ? km/h |
| Stall Speed * | 104 km/h (estimated) |
Service Ceiling | 10900 m |
| Rate of Climb | 15.24 m/s |
Range | 2280 km |
(*) vitesse de décrochage
| Sources | |||
| Wikipédia | Military Factory | ||
Drawings |
