Myasishchev M-60

The Myasishchev M-60 was a Soviet design for a nuclear-powered bomber.[1] The design was similar to the M-50 bomber prototype.

Myasishchev received the instruction to start the development of the M-60 on 19 May 1955. However, it did not make it out of the planning stage, and the M-60 program was cancelled in 1959.[1][2]

It appears that the M-60 designation has been used for a number of projects at Myasishchev,[3] including a recent transport and civil aircraft.[4]

Model of the Aircraft

Specifications (M-60)

  • Role: Strategic Bomber / Flying Atomic Laboratory
  • Crew: 2 (housed in a massive 60-ton lead-shielded capsule for radiation protection)
  • Propulsion: 4 x Lulka nuclear-powered turbojets
  • Alternative setup: 2 nuclear engines for cruise and 2 conventional chemical turbojets for takeoff/landing


Performance (Estimated):

  • Max Speed: Mach 2 (approx. 2,000+ km/h)
  • Range: 25,000 km
  • Service Ceiling: 16,500 – 20,000 m


Dimensions:

  • Length: ≈59.5 m (195 ft)
  • Wingspan: ≈24 m (78 ft)
  • Take-off Weight: ≈136,000 kg (300,000 lbs)

See also

Aircraft of comparable role, configuration, and era

References

Notes
  1. 1 2 Trakimavičius, Lukas. "The Future Role of Nuclear Propulsion in the Military" (PDF). NATO Energy Security Centre of Excellence. Archived from the original (PDF) on 2021-10-18. Retrieved 2021-10-15.
  2. ↑ Colon 2009
  3. ↑ Buttler & Gordon 2004, pp. 81–82
  4. ↑ ATO Russia & CIS Observer Deprecated link archived 2012-07-20 at archive.today
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