Myasishchev M-50 Bounder

✈️ Aircraft Specifications

DesignationM-50
ManufacturerMyasishchev
Country of OriginSoviet Union
First Flight1959
Length57.48 m (188.6 ft)
Max Speed (Mach)1.59
Max Speed (km/h)1,950 km/h
Service Ceiling16,500 m (54,137 ft)
Range7,400 km (4,595 mi)
Engine2× Dobrynin VD-7F + 2× Dobrynin VD-7 turbojet
Crew2
StatusPrototype

Overview

The Myasishchev M-50 (NATO reporting name “Bounder”) is a Soviet prototype four-engine supersonic strategic bomber that never entered service. First flown on 27 October 1959, this enormous aircraft — nearly 58 meters long — was designed to deliver nuclear weapons at supersonic speeds across intercontinental distances. Only one flight-worthy prototype was built before the program was terminated in favor of intercontinental ballistic missiles.

Design & Development

The M-50 was designed by the Myasishchev bureau as an intercontinental supersonic bomber. It featured four engines in an unusual configuration: two Dobrynin VD-7F afterburning turbojets mounted under the shoulder-mounted truncated delta wings, and two non-afterburning VD-7 turbojets at the wingtips. The shoulder-mounted delta wing design was optimized for supersonic cruise.

A second aircraft, designated M-52, was also developed with Zubets 16-17 turbofan engines and a redesigned wider cockpit with side-by-side seating replacing the M-50’s tandem arrangement. An unmanned M-51 intercontinental cruise missile variant was also proposed for delivering multiple warheads to targets in the United States.

Operational History

The M-50 made its first flight on 27 October 1959 and completed 19 flights in total. Its sole public appearance came on 9 July 1961 during a flypast at the annual Tushino air show — Soviet Aviation Day. This dramatic appearance stunned Western observers, who initially believed the bomber might be nuclear-powered based on a 1958 Aviation Week article. The M-52 was completed but never flight-tested.

Like most early 1960s supersonic strategic bomber programs worldwide, the M-50/52 was terminated as ICBMs proved more cost-effective and survivable for nuclear delivery. The Soviet space program also absorbed resources and political attention. The sole M-50 prototype survives on display at the Monino Museum outside Moscow.

Capabilities

  • Maximum Speed: 1,950 km/h (Mach 1.59 / 1,210 mph)
  • Service Ceiling: 16,500 m (54,100 ft)
  • Range: 7,400 km (4,600 mi)
  • Length: 57.48 m (188 ft 7 in) — massive airframe
  • Maximum Takeoff Weight: 200,000 kg (440,925 lb)
  • Engines: 2× VD-7F afterburning + 2× VD-7 non-afterburning turbojets

Armament & Weapons

  • Internal Bomb Bay: Up to 30,000 kg (66,000 lb) of bombs or missiles
  • Cruise Missiles: M-59 and M-61 long-range cruise missiles
  • Nuclear Delivery: Designed primarily for nuclear weapon delivery

Video

Frequently Asked Questions

Was the M-50 nuclear-powered?

No. A 1958 Aviation Week article falsely claimed the Soviets were flight-testing a nuclear-powered bomber, and photographs of the M-50 were mistakenly associated with this claim. The M-50 was powered by conventional turbojet engines.

How big was the M-50?

The M-50 was enormous — nearly 58 meters (190 feet) long with a wingspan of 25 meters and a maximum takeoff weight of 200 tonnes. It remains one of the largest combat aircraft ever designed.

Why was the M-50 cancelled?

The development of reliable ICBMs made manned supersonic strategic bombers seem unnecessary and far more expensive per nuclear delivery capability. Resources were redirected to the Soviet missile and space programs.

References & Sources

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