Yakovlev Yak-60

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This article is about a conjectural designation for a helicopter project. For the Yakovlev izdeliye 60 (изделие, "item") reconnaissance drone, see Yakovlev Pchela.

Yakovlev Yak-60 is the possible designation for an experimental Yakovlev tandem-rotor heavy-lift helicopter design of the late 1960s. This design never progressed beyond the model stage.[1]


This helicopter was designed in the late 1960s, and may have been a competing design to the Mi-12 heavy lift helicopter. It featured two Mi-6 rotors in tandem, each driven by a pair of 6,500shp D-25VF engines, potentially giving it four times the payload capacity of the Boeing Vertol Chinook. The cockpit would have been similar to that of the Yak-24. Compared to the radical Mi-12, the Yak-60 design was far more conventional, though ultimately two Mi-12s were produced.[1]

The designation Yak-60 has been suggested based on an extant study model which has the number "60" painted prominently on its side.[1]

Specifications (Yak-60)[edit]

General characteristics

  • Crew: three
  • Capacity: 42 tonnes (92,593 lb) of cargo
  • Length: 46 m (150 ft 0 in)
  • Wingspan: 2x 35 m (115 ft 0 in)
  • Height: m (ft)
  • Empty weight: 55,000 kg (120,000 lb)
  • Max. takeoff weight: 100,000 kg (220,000 lb)
  • Powerplant: 2 × 4 X D-25VF radials, 26,000shp () each



  1. ^ a b c Gunston, 1997
  • Gunston, Bill. Yakovlev Aircraft since 1924. London, UK: Putnam Aeronautical Books, 1997. ISBN 1-55750-978-6.