About DBkWik

About: dbkwik:resource/U6lBmy6_yky4bSdYuR3S-g==

PropertyValue
rdf:type
rdfs:label
  • Yakovlev UT-2
rdfs:comment
  • 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.
  • {| |} The Yakovlev UT-2 (, NATO reporting name "Mink") was a trainer aircraft used by the Soviet Air Force from 1937 until the 1950s. It was the standard Soviet trainer during World War II.
  • The Yakovlev UT-2 (Russian: УТ-2, NATO reporting name "Mink") was a trainer aircraft used by the Soviet Air Force from 1937 until the 1950s. It was the standard Soviet trainer during World War II.
owl:sameAs
empty weight kg
  • 628
Length
  • 7.0
dcterms:subject
dbkwik:military/property/wikiPageUsesTemplate
dbkwik:world-war-2/property/wikiPageUsesTemplate
dbkwik:world-war-two/property/wikiPageUsesTemplate
dbkwik:worldwartwo/property/wikiPageUsesTemplate
Range
  • 750.0
range km
  • 1130
ceiling ft
  • 16400
climb rate ftmin
  • 649
emptyweight
  • 616.0
Speed
  • 200.0
met or eng?
  • met
range miles
  • 702
Affiliation
eng1 type
  • Shvetsov M-11D
gross weight kg
  • 940
length in
  • 5
Name
  • Yakovlev UT-2MV
Type
  • Light Bomber
  • Trainer/Fighter-trainer
eng1 kW
  • 93.200000
wing area sqft
  • 184.300000
height m
  • 2.990000
Height in
  • 10
span m
  • 10.200000
climb rate ms
  • 3.300000
Manufacturer
max speed kmh
  • 210
empty weight lb
  • 1385
ceiling m
  • 5000
cruise speed kmh
  • 99
length m
  • 7.150000
max speed mph
  • 131
National Origin
  • USSR
length ft
  • 23
Developed From
  • AIR-10, Ya-20
Height ft
  • 9
First Flight
  • --07-11
span ft
  • 33
cruise speed mph
  • 60
gross weight lb
  • 2073
span in
  • 5
Engine
  • Shvetsov M-11E Engine
wing area sqm
  • 17.120000
Crew
  • 2
Armament
  • 2
  • 4
Number Built
  • 7243
Year
  • 1937
eng1 hp
  • 125
Designer
ref
  • Gordon 2005, and Gunston 1995
eng1 number
  • 1
abstract
  • 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.
  • {| |} The Yakovlev UT-2 (, NATO reporting name "Mink") was a trainer aircraft used by the Soviet Air Force from 1937 until the 1950s. It was the standard Soviet trainer during World War II.
  • The Yakovlev UT-2 (Russian: УТ-2, NATO reporting name "Mink") was a trainer aircraft used by the Soviet Air Force from 1937 until the 1950s. It was the standard Soviet trainer during World War II.