Statements (34)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:alsoKnownAs |
UT-2
|
| gptkbp:category |
low-wing aircraft
single-engine aircraft 1930s Soviet military trainer aircraft |
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:crew |
2
|
| gptkbp:emptyWeight |
730 kg
|
| gptkbp:engineType |
gptkb:piston_engine
|
| gptkbp:firstFlight |
1935
|
| gptkbp:height |
2.7 m
|
| gptkbp:introduced |
1937
|
| gptkbp:length |
7.3 m
|
| gptkbp:manufacturer |
gptkb:Yakovlev
|
| gptkbp:maximumSpeed |
210 km/h
|
| gptkbp:maxTakeoffWeight |
1,050 kg
|
| gptkbp:numberBuilt |
7243
|
| gptkbp:primaryUser |
gptkb:Soviet_Air_Force
|
| gptkbp:range |
500 km
|
| gptkbp:retired |
1950s
|
| gptkbp:role |
gptkb:trainer_aircraft
|
| gptkbp:serviceCeiling |
4,000 m
|
| gptkbp:successor |
gptkb:Yakovlev_Yak-18
|
| gptkbp:usedInConflict |
gptkb:World_War_II
|
| gptkbp:variant |
UT-2L
UT-2M UT-2MV |
| gptkbp:wingspan |
10.2 m
|
| gptkbp:bfsParent |
gptkb:Royal_Mongolian_Air_Force
gptkb:Shvetsov_M-11_radial_engine gptkb:Shvetsov_M-11FR gptkb:World_War_II_trainer_aircraft |
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Yakovlev UT-2
|