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Yakovlev Yak-8

Military Aircraft

The Yakovlev Yak-8 was a Soviet utility transport developed during the Second World War as an enlarged development of the Yak-6. It kept the mixed construction of its predecessor, with a plywood-skinned wooden forward and central fuselage, a fabric-covered tubular steel rear fuselage and a two-spar wooden wing, but its deeper fuselage gave headroom for six passengers instead of four. Two 190 hp Kossov M-12 engines were intended, yet they were unavailable and two 145 hp Shvetsov M-11FM radials were used. Two prototypes were built, the first flying in early 1944. The lighter second prototype passed State acceptance tests and was recommended for production but never ordered, probably because the Soviets were switching to all-metal aircraft, although it still received the NATO reporting name Crib.

Facts
Year
1944 1
Engine Class
Piston 1
Status
Prototype 1
Units Built
2 1
Top Speed (km/h)
248 1
Mass (kg)
1750 1
Maximum Mass (kg)
2700 1
Engine
Shvetsov M-11FM single-row, five-cylinder, air-cooled radial engine 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Yakovlev Yak-8 (Wikipedia)

Of Make

Source Yakovlev Yak-8 (Wikipedia)
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Source Yakovlev Yak-8 (Wikipedia)Lead
Quote, Lead
The Yakovlev Yak-8 was a Soviet utility aircraft developed during World War II.

Originated In

Also in Geography Atlas: where this subject originated.

Source Yakovlev Yak-8 (Wikipedia)Lead
Quote, Lead
The Yakovlev Yak-8 was a Soviet utility aircraft developed during World War II.
Sources
1. Yakovlev Yak-8 (Wikipedia)
  • Lead
    The Yakovlev Yak-8 was a Soviet utility aircraft developed during World War II.
  • Development, first flight
    Two prototypes were built with the first flying in early 1944
  • Specifications, powerplant
    Powerplant: 2 × Shvetsov M-11FM single-row, five-cylinder, air-cooled radial engine
  • Specifications, engine fitted
    Powerplant: 2 × Shvetsov M-11FM single-row, five-cylinder, air-cooled radial engine
  • Specifications, empty weight
    Empty weight: 1,750 kg
  • Specifications, maximum weight
    Max takeoff weight: 2,700 kg
  • Specifications, maximum speed
    Maximum speed: 248 km/h
  • Status
    Two prototypes were built with the first flying in early 1944
  • Production, number built
    Two prototypes were built
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