The Yakovlev UT-2 had a Shvetsov M-11E Engine that was capable of propelling it at a maximum speed of up to 200 km/h. The UT-2 was designed to be a faster and more effective trainer than the elder Polikarpov Po-2 for teaching Soviet pilots how to fly more modern aircraft such as the Lavochkin La-5 or Yakovlev Yak-9. The total weight of the aircraft was around 616 kilograms empty while its total length was about 7.0 meters. The operational range of the aircraft was around 750 kilometers with a service ceiling of 5,000 meters.
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empty weight kg |
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Length |
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Range |
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range km |
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ceiling ft |
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climb rate ftmin |
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emptyweight |
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Speed |
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met or eng? |
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range miles |
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Affiliation | |
eng1 type |
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gross weight kg |
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length in |
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Type |
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eng1 kW |
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wing area sqft |
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height m |
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Height in |
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span m |
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climb rate ms |
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Manufacturer | |
max speed kmh |
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empty weight lb |
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ceiling m |
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cruise speed kmh |
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length m |
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max speed mph |
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National Origin |
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length ft |
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Developed From |
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Height ft |
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First Flight |
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span ft |
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cruise speed mph |
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gross weight lb |
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span in |
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Engine |
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wing area sqm |
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Crew |
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Armament |
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Number Built |
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Year |
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eng1 hp |
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eng1 number |
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abstract |
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