About: Alekseyev I-212   Sponge Permalink

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

The Alekseyev I-212 was a twin-engined, jet fighter designed in the USSR in 1947 by Experimental Design Bureau 21 (OKB). It was a two-seat variant of the I-21 (Istrebitel' - Fighter) that had been designed in response to a requirement for a very long-range fighter issued by the Soviet Air Forces in 1946. Intended as an escort fighter, it was also designed for use as a night fighter and reconnaissance aircraft. Sources are contradictory about the construction of a prototype, but it is known that the aircraft never flew.

AttributesValues
rdf:type
rdfs:label
  • Alekseyev I-212
rdfs:comment
  • The Alekseyev I-212 was a twin-engined, jet fighter designed in the USSR in 1947 by Experimental Design Bureau 21 (OKB). It was a two-seat variant of the I-21 (Istrebitel' - Fighter) that had been designed in response to a requirement for a very long-range fighter issued by the Soviet Air Forces in 1946. Intended as an escort fighter, it was also designed for use as a night fighter and reconnaissance aircraft. Sources are contradictory about the construction of a prototype, but it is known that the aircraft never flew.
sameAs
dcterms:subject
dbkwik:military/pr...iPageUsesTemplate
max takeoff weight alt
  • 23148.0
loaded weight main
  • 9250.0
Guns
  • 2(xsd:integer)
  • forward-facing: 1 × 37 mm Nudelman N-37 cannon and 2 × 23 mm Nudelman-Suranov NS-23 cannon.
climb rate main
  • 29.76
length alt
  • 1308.1000000000001
span main
  • 16.2 m
thrust alt
  • 4916(xsd:integer)
Type
range alt
  • 1429.0
length main
  • 13.08 m
area main
  • 33.0
ferry range main
  • 3100.0
span alt
  • 53(xsd:integer)
range main
  • 2300.0
Manufacturer
max speed main
  • 1000(xsd:integer)
climb rate alt
  • 5858.0
ceiling main
  • 14,800 m
National Origin
  • USSR
type of jet
  • RD-45
loaded weight alt
  • 20393.0
Developed From
  • Alekseyev I-21
area alt
  • 355.0
engine (jet)
  • centrifugal flow turbojet
max speed alt
  • 621.0
jet or prop?
  • jet
ferry range alt
  • 1926.0
thrust main
  • 2230(xsd:integer)
number of jets
  • 2(xsd:integer)
plane or copter?
  • plane
ceiling alt
  • 48560.0
max takeoff weight main
  • 10500.0
Crew
  • 2(xsd:integer)
Designer
ref
  • The Osprey Encyclopedia of Russian Aircraft 1875-1995, p. 17
abstract
  • The Alekseyev I-212 was a twin-engined, jet fighter designed in the USSR in 1947 by Experimental Design Bureau 21 (OKB). It was a two-seat variant of the I-21 (Istrebitel' - Fighter) that had been designed in response to a requirement for a very long-range fighter issued by the Soviet Air Forces in 1946. Intended as an escort fighter, it was also designed for use as a night fighter and reconnaissance aircraft. Sources are contradictory about the construction of a prototype, but it is known that the aircraft never flew.
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