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UT-1 | ||
Training aircraft | ||
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Specification: | |
Year deployed
Wing span, m Lenght, m Height, m Wings area, m2 Weight, kg - empty aircraft - normal take-off Engine Power, hp Maximum speed, km/h Cruising speed, km/h Range, km Rate of climb, m/min Service ceiling, m Crew |
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1937 - 7.30 - 5.75 - 2.34 - 9.58 - 420 - 590 - 1 PE M-11 (M-11E) - 1 У 100 (150) - 249 - 212 - 670 - 300 - 6180 - 1 |