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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| Name |
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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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| Designer | |
| ref |
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| eng1 number |
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| abstract |
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