About: Yatsenko I-28   Sponge Permalink

An Entity of Type : dbkwik:resource/AGhloO_nVTaFp7GvOmHv5Q==, within Data Space : 134.155.108.49:8890 associated with source dataset(s)

{| |} The Yatsenko I-28 was a 1930s Soviet single-seat fighter designed by Vladmir Yatsenko and first flown in 1939. The I-28 was a low-wing cantilever monoplane of mixed construction powered by a Tumansky M-87 radial piston engine. It had an enclosed single-seat cockpit with a rearwards sliding canopy. The wing had an inverted-gull shape to reduce the length of the retractable main landing legs. The prototype was destroyed shortly after the first flight but an order was placed for 30 production aircraft. Also ordered was a prototype of an attack version, the I-28Sh. Although the first five production aircraft were completed the programme was cancelled in early 1940.

AttributesValues
rdf:type
rdfs:label
  • Yatsenko I-28
rdfs:comment
  • {| |} The Yatsenko I-28 was a 1930s Soviet single-seat fighter designed by Vladmir Yatsenko and first flown in 1939. The I-28 was a low-wing cantilever monoplane of mixed construction powered by a Tumansky M-87 radial piston engine. It had an enclosed single-seat cockpit with a rearwards sliding canopy. The wing had an inverted-gull shape to reduce the length of the retractable main landing legs. The prototype was destroyed shortly after the first flight but an order was placed for 30 production aircraft. Also ordered was a prototype of an attack version, the I-28Sh. Although the first five production aircraft were completed the programme was cancelled in early 1940.
sameAs
empty weight kg
  • 1850(xsd:integer)
dcterms:subject
dbkwik:military/pr...iPageUsesTemplate
range km
  • 800(xsd:integer)
ceiling ft
  • 35600(xsd:integer)
met or eng?
  • met
range miles
  • 497(xsd:integer)
eng1 type
  • Tumansky M-87B radial piston engine
gross weight kg
  • 2720(xsd:integer)
length in
  • 0(xsd:integer)
Type
  • Single-seat fighter
eng1 kW
  • 820(xsd:integer)
wing area sqft
  • 178(xsd:integer)
span m
  • 9(xsd:double)
Manufacturer
  • Yatsenko OKB
max speed kmh
  • 576(xsd:integer)
empty weight lb
  • 4079(xsd:integer)
ceiling m
  • 10800(xsd:integer)
length m
  • 8(xsd:double)
max speed mph
  • 359(xsd:integer)
National Origin
length ft
  • 28(xsd:integer)
First Flight
  • 1939-06-10(xsd:date)
span ft
  • 31(xsd:integer)
gross weight lb
  • 5997(xsd:integer)
span in
  • 6(xsd:integer)
wing area sqm
  • 16(xsd:double)
Crew
  • 1(xsd:integer)
Armament
  • two cannons and one machine gun
Number Built
  • 7(xsd:integer)
eng1 hp
  • 1100(xsd:integer)
Designer
ref
  • (The History of Soviet Aircraft from 1918 )
eng1 number
  • 1(xsd:integer)
abstract
  • {| |} The Yatsenko I-28 was a 1930s Soviet single-seat fighter designed by Vladmir Yatsenko and first flown in 1939. The I-28 was a low-wing cantilever monoplane of mixed construction powered by a Tumansky M-87 radial piston engine. It had an enclosed single-seat cockpit with a rearwards sliding canopy. The wing had an inverted-gull shape to reduce the length of the retractable main landing legs. The prototype was destroyed shortly after the first flight but an order was placed for 30 production aircraft. Also ordered was a prototype of an attack version, the I-28Sh. Although the first five production aircraft were completed the programme was cancelled in early 1940.
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