(Myasishchev) M-4 & 3M Bison @·AIRCRAFTUBE

  • Myasishchev 3M Bison
Myasishchev 3M Bison
    Myasishchev 3M Bison
  • Myasishchev 3M Bison-B
Myasishchev 3M Bison-B
    Myasishchev 3M Bison-B
  • 3M Bison - 1968
3M Bison - 1968
    3M Bison - 1968
  • Bison 3M - Tomcat VF-102 intercept c1983
Bison 3M - Tomcat VF-102 intercept c1983
    Bison 3M - Tomcat VF-102 intercept c1983
  • Myasishchev 3MD - VVS museum
Myasishchev 3MD - VVS museum
    Myasishchev 3MD - VVS museum
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Myasishchev M-4
    Myasishchev M-4
  • Myasishchev M-4
Myasishchev M-4
    Myasishchev M-4
  • Myasishchev M-4 Bison
Myasishchev M-4 Bison
    Myasishchev M-4 Bison
  • Myasishchev M-4
Myasishchev M-4
    Myasishchev M-4
  • Myasishchev M-4
Myasishchev M-4
    Myasishchev M-4
  • Myasishchev M-4 Bison 1982
Myasishchev M-4 Bison 1982
    Myasishchev M-4 Bison 1982
  • Myasishchev M-4
Myasishchev M-4
    Myasishchev M-4
  • Myasishchev_M-4 Bison
Myasishchev_M-4 Bison
    Myasishchev_M-4 Bison
  • Myasishchev VM-T Atlant
Myasishchev VM-T Atlant
    Myasishchev VM-T Atlant
  • Myasishchev VM-T Atlant - MAKS 2005
Myasishchev VM-T Atlant - MAKS 2005
    Myasishchev VM-T Atlant - MAKS 2005
  • Myasishchev VM-T Atlant Myasishchev VM-T Atlant
    Myasishchev VM-T Atlant

Myasishchev M-4 and 3M 'Bison'

Myasishchev M-4

The end of second world war is marked by the apparition of the atomic bomb both in Russia and the United States. As the need to deliver this new weapon at high speed over long distances could not be fulfilled by the piston engined bombers of the time, (The Boeing B-29 and its copy, the Tupolev Tu-4) both sides began studies on heavy jet bombers. This led to the apparition of planes like the B-47 and B-52, the Russians producing a very similar machine, the Miyassichtchev M-4, (NATO code 'Bison').

Unfortunately, the M-4 never completely fulfilled the criteria for which it had been designed, mainly because of its short range. Jet engines of that time were still far from offering good reliability and low weight, together with high thrust and a good Specific Fuel Consumption (or SFC). Nonetheless, the impressing number of innovations the M-4 integrated testifies of the many efforts and problems encountered in the design of this new generation of heavy jets : Landing gear integrated to the fuselage, high elongation swept wings, in flight refuelling. . .

The first flight of the M-25 prototype took place on the 20th of January, 1953, with pilots F. Opadchiy and A. Gratzyansky at the controls, less then two years after the project was launched.

The second prototype brought many modifications, the most spectacular being the mounting of a jack that automatically increased front gear extension when take-off speed had been reached, modifying the wing's angle of attack for lift-off. Normal rotation technique would indeed have been impossible as the rear main gear was positioned way aft the center of gravity. This system caused a lot of accidents at the beginning of the operations, mainly because of the lack of experience pilots had on this system.

Produced from 1954 to 1956, the M-4 was later used for reconnaissance and for in flight refuelling. Engines were then 21,000 lbf Mikulin AM-3M's.

Myasishchev 3M

This version is a development of the M-4 with reduced payload (18 tons instead of 24), smaller dimensions and improved aerodynamics.

The 3M made its first flight on the 27th of march, 1956, piloted by M. Gallaï and N. Goryainov. At this time, the VD-7 engines were only at the start of their production and still had many problems to be fixed, so the flight was made with two VD-7 on one side and two AM-3 on the other.

Testing was not yet finished when production of the first aircraft started. Catastrophe was avoided many times during this period, mainly because of the poor reliability and stability of the engines.

With wings conceived to disperse radio waves, the 3M is the first Russian bomber with stealth technology. The variable pitch stabiliser is also a main modification that was introduced during production.

The 3M, nicknamed 'Troïka', beat many world records in 1959 : Speed record on a 1,000 km distance and records for bringing high loads at high altitude.

Production stopped abruptly in the early sixties, the resources of 'Plant 23' near Moscow being urgently re-organised in favour of the design and construction of the new concept of ballistic missiles. Overhauls and modifications on existing models took place at the Ryazan plant from that period.

In the eighties and until 1994, the 3M was mainly used as a tanker. All versions included, 75 Troïka were built from 1956 till 1959.

Myasishchev VM-T 'Atlant'

The 3M's career ends with the modification of two machines into heavy external load carriers. They were planned for transportation of elements of the Bourane space shuttle and of the Energia rocket. For that purpose, new VD-7MD engines were installed, the tail was modified into a double fin and many structural reinforcements were added. The Atlant first flew in April 1981.

Versions :

  • 3MC : RD-3M-500 engines.
  • 3MC-I : Bomber.
  • 3MC-II : Tanker version of the 3MC.
  • 3MD : New avionics. The last bomber version. 11 exemplars built.
  • 3ME : Unique version. Increased wing area, new electronics.
  • 3MH, 3MN-I and 3MN-II : VD-7B engines.
  • 3MH-I : Bomber.
  • 3MH-II : Tanker version of the 3MH.
  • 3M-5 : Study on a platform for two KSR-5 missiles. New "Rubin 1ME" radar and "Azalia" ECM system (1972).
  • 3MP : Polyvalent version : Bomber or tanker.
  • 3MT : Tanker. Later transformed for extreme load transportation.

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This text stays momentarily aircraftube.com©´s property, before its full or partial integration to Wikipedia.

Specifications (3MD)

  • Crew : 7.
  • Length : 169 ft 11 in (51.8 m).
  • Height : 37 ft 8 in (11.5 m).
  • Wing span : 174 ft 4 in (53.14 m).
  • Wing area : 3,875 sq ft (360 m²).
  • Gross weight : 418,880 lb (190,000 kg).
  • Empty weight : 169,316 lb (76,800 kg).
  • Max payload : 39,680 lb (18 tons) of bombs.
  • Max Speed : 575 mph (500 kts - 926 km/h) at 27,887 ft (8,500 m).
  • Service ceiling : 39,862 ft (12,150 m).
  • Max range : 6,711 mi (5,832 nm - 10,800 km).
  • Engines : VD-7B.
  • Thrust : 20,943 lbf (93.16 kN) per engine.
  • Armament : Six 23 mm guns.

Specifications (M-4)

  • Crew : 8.
  • Length : 156 ft 4 in (47.65 m).
  • Height : 37 ft 6 in (11.43 m).
  • Wing span : 165 ft 8 in (50.5 m).
  • Wing area : 3,563 sq ft (331 m²).
  • Gross weight : 405,653 lb (184,000 kg).
  • Max landing weight : 220,463 lb (100,000 kg).
  • Empty weight : 167,993 lb (76,200 kg).
  • Max payload : 52,911 lb (24,000 kg).
  • Max Speed : 590 mph (513 kts - 950 km/h) at 21,982 ft (6,700 m).
  • Service ceiling : 37,073 ft (11,300 m).
  • Max range : 5,654 mi (4,913 nm - 9,099 km).
  • Engines : Four Mikulin AM-3A.
  • Thrust : 19,181 lbf (85.32 kN).

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This text stays momentarily aircraftube.com©´s property, before its full or partial integration to Wikipedia.
Myasishchev M-4 & 3M Molot (Bison) : Your comments on this subject
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