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Bombers ·Myasishchev

M-4 Bison

Soviet strategic bomber, renowned for its Cold War service, extensively deployed for long-range maritime reconnaissance and bombing missions. Key figures: top speed 947 km/h, range 5,600 km, service ceiling 11,000 m, max takeoff weight 181,500 kg, unit price $8M, built 123.

Max speed
947km/h
Range
5,600km
Produced
123units
Avg unit price
$8 million
Myasishchev M-4 Bison bombers side profile drawing
Side profile · Myasishchev M-4 Bison · length 47.2 m
Technical SpecificationsVersion: M-4 Bison-A
Crew7
Length47.2 m (154.9 ft)
Wingspan50.5 m (165.7 ft)
Height14.1 m (46.3 ft)
Wing area326.4 m² (3512.8 sqft)
Empty weight79,700 kg (175,708 lbs)
Max. takeoff weight181,500 kg (400,139 lbs)
Powerplant4 × turbojets Mikouline AM-3 9,525 kgf each
PerformanceVersion: M-4 Bison-A
Maximum speed947 km/h (588 mph)
Operational range5,600 km (3,480 mi)
Service ceiling11,000 m (36,089 ft)
Operators — 2026
No country is operating the M-4 Bison in 2026.
Armament
Bombs payload
All Operators
🇷🇺 Russia· 🇷🇺 Ex-USSR

Description

Designed as a strategic nuclear bomber in the 1950s, shortly after the B-52 Stratofortress, the M-4 Bison was a quadruplex bomber designed in response to the Soviet Union's need for a bomber force capable of reaching the continental United States. From the beginning, it was hindered by a range too short to carry out intercontinental missions for which it was intended.

Development

The first prototype of the M-4 made its first flight on January 20, 1953, and the state acceptance tests were conducted in March 1954. Serial production began the same year, and the aircraft entered service in 1955. A total of 34 aircraft were built, including two prototypes.

Design

The M-4 had a swept wing with a 35 degrees angle and was mainly constructed with aluminum alloys, with some steel and magnesium components. It was powered by four Mikulin AM-3A engines, later replaced by RD-3M-500 turbojet engines. Despite a fuel capacity of 123,600 liters, the range of the initial M-4/2M version was only 8,000 km due to fuel-thirsty engines, which prevented it from having strategic bombing capabilities. Even after engine changes, the M-4/2M version never managed to overcome this problem, and it was not until the 3M/M-6 (Bison B) version that the range increased to 11,800 km due to increased fuel capacity and new fuel-efficient and more powerful engines.

Armament

The bomber was equipped with 23mm AM-23 cannons for self-defense, with a dual-purpose tail turret and two remotely operated turrets located in the upper and lower parts of the fuselage. It could carry a payload of 24 tons in different configurations.

The M-4 Bison was operated by a crew of eight people, including a navigator/bombardier, a pilot, a co-pilot, a radar/navigator operator, a flight engineer/gunner, a radio operator/gunner, a dorsal turret gunner, and a tail turret gunner for self-defense.

Operational History

The M-4 was used by the Soviet Union for several decades, and 200 aircraft were reportedly built. The bombing versions were retired in the early 1980s in response to the START 1 agreements on nuclear disarmament. The aerial refueling versions remained in service until 1994.

Variants

Developed versions include:

  • Bison A - M-4/2M: Strategic nuclear bombing version.

  • Bison B - 3M/M-6: Improved version of the strategic nuclear bomber with increased fuel capacity and new engines, four VD-7 engines. Aerial refueling capability.

  • Bison B - 3MS/M-6: Strategic nuclear bombing version equipped with new RD-3M-500A engines. A version designated 3MS2 was specifically developed for aerial refueling, yet retained the NATO code Bison-B.

  • Bison C - 3MD/M-6/3MN: Strategic nuclear bombing version with new VD-7B engines. This version also had aerial refueling capability.

  • Bison C - 3MN-2: Aerial refueling version derived from the 3MD model.

  • Project 28: Study for a high-altitude bombing version. The project was not completed.

  • 3M-T/BM-T "Atlant": An aircraft converted for the transport of Energia rocket components.

Wikipedia (CC BY-SA) and other open sources. Illustrations generated by AI. Last updated on 1 August 2026. Suggest a change

Frequently Asked Questions

What type of aircraft is the M-4 Bison?
The Myasishchev M-4 Bison is a bombers aircraft developed by Myasishchev and entered service in 1953.
What is the maximum speed of the M-4 Bison?
The Myasishchev M-4 Bison has a maximum speed of 947 km/h (588 mph).
What is the range of the M-4 Bison?
The Myasishchev M-4 Bison has an operational range of 5,600 km (3,479 miles). This range can vary based on payload, altitude, and mission profile.
When did the M-4 Bison first fly?
The Myasishchev M-4 Bison made its first flight on January 20, 1953. It entered operational service in 1953.
How many M-4 Bison have been built?
Approximately 123 units of the Myasishchev M-4 Bison have been produced since it entered service in 1953.
How much does a M-4 Bison cost?
The Myasishchev M-4 Bison has an estimated unit cost of approximately $8.0 million. Actual prices vary based on configuration, quantity ordered, and included support packages.
What is the service ceiling of the M-4 Bison?
The Myasishchev M-4 Bison has a service ceiling of 11,000 meters (36,089 feet). This is the maximum altitude at which the aircraft can maintain controlled flight.
Compare This Aircraft
M-4 Bison vs
Latest Data Updates
  1. AUG 12026 Updated Manufacturer updated
  2. JUL 232026 Updated Sources and cross-references refreshed
  3. APR 72026 Updated Sources and cross-references refreshed
  4. JAN 122026 Updated Range updated in a site-wide editorial pass