Myasishchev VB-109
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The Myasishchev DB-108 was a 1940s Soviet experimental development of the
Petlyakov Pe-2 The Petlyakov Pe-2 (russian: Петляков Пе-2) was a Soviet twin-engine dive bomber used during World War II. One of the outstanding tactical attack aircraft of the war,Ethell 1996, p. 152. it also proved successful as a heavy fighter, as ...
bomber aircraft. Only three prototypes were built and only two of them flew.


Design and development

After
Vladimir Petlyakov Vladimir Mikhailovich Petlyakov (russian: Влади́мир Миха́йлович Петляко́в; 15 June 1891 – 12 January 1942) was a Soviet aeronautical engineer and aircraft designer. Petlyakov was born in 1891 in Sambek (Don Host O ...
's death in January 1942
Vladimir Mikhailovich Myasishchev Vladimir Mikhailovich Myasishchev (russian: Владимир Михайлович Мясищев) (September 28, 1902 in Yefremov (town), Yefremov – October 14, 1978 in Moscow) was a Soviet Union, Soviet aircraft designer, Major General of Eng ...
continued the development of the Petlyakov Pe-2, beginning with the DB-108. DB stood for long range bomber and 108 was a
NKVD The People's Commissariat for Internal Affairs (russian: Наро́дный комиссариа́т вну́тренних дел, Naródnyy komissariát vnútrennikh del, ), abbreviated NKVD ( ), was the interior ministry of the Soviet Union. ...
, rather than design bureau, number. The three prototypes were identified by their designer's initials, VM. All three had the same basic layout. Their
cantilever A cantilever is a rigid structural element that extends horizontally and is supported at only one end. Typically it extends from a flat vertical surface such as a wall, to which it must be firmly attached. Like other structural elements, a canti ...
wings were mid-mounted and had rectangular panels between roots and engines, with radiators in their
leading edge The leading edge of an airfoil surface such as a wing is its foremost edge and is therefore the part which first meets the oncoming air.Crane, Dale: ''Dictionary of Aeronautical Terms, third edition'', page 305. Aviation Supplies & Academics, ...
s. The engines were mounted ahead of the
leading edge The leading edge of an airfoil surface such as a wing is its foremost edge and is therefore the part which first meets the oncoming air.Crane, Dale: ''Dictionary of Aeronautical Terms, third edition'', page 305. Aviation Supplies & Academics, ...
s in long fairings that also housed the main
landing gear Landing gear is the undercarriage of an aircraft or spacecraft that is used for takeoff or landing. For aircraft it is generally needed for both. It was also formerly called ''alighting gear'' by some manufacturers, such as the Glenn L. Martin ...
. The oil radiators were nearby in the leading edges of the outer wing panels which tapered strongly to semi-elliptical tips and had about 5° dihedral. Their fuselages were oval in cross-section and tapered rearwards to pointed extremities. Each had a glazed or semi-glazed nose and a cockpit, under raised, multi-part glazing, placed ahead of the leading edge. At the rear tetragonal plan, mid-mounted
tailplane A tailplane, also known as a horizontal stabiliser, is a small lifting surface located on the tail (empennage) behind the main lifting surfaces of a fixed-wing aircraft as well as other non-fixed-wing aircraft such as helicopters and gyroplane ...
s with marked dihedral carried vertical endplate
fin A fin is a thin component or appendage attached to a larger body or structure. Fins typically function as foils that produce lift or thrust, or provide the ability to steer or stabilize motion while traveling in water, air, or other fluids. Fin ...
s which, with their
rudder A rudder is a primary control surface used to steer a ship, boat, submarine, hovercraft, aircraft, or other vehicle that moves through a fluid medium (generally aircraft, air or watercraft, water). On an aircraft the rudder is used primarily to ...
s, were roughly oval in profile. The
trailing edge The trailing edge of an aerodynamic surface such as a wing is its rear edge, where the airflow separated by the leading edge meets.Crane, Dale: ''Dictionary of Aeronautical Terms, third edition'', page 521. Aviation Supplies & Academics, 1997. ...
s of broad chord
elevators An elevator or lift is a cable-assisted, hydraulic cylinder-assisted, or roller-track assisted machine that vertically transports people or freight between floors, levels, or decks of a building, vessel, or other structure. They are ...
were slightly curved, with inboard
trim tabs Trim tabs are small surfaces connected to the trailing edge of a larger control surface on a boat or aircraft, used to control the trim of the controls, i.e. to counteract hydro- or aerodynamic forces and stabilise the boat or aircraft in a pa ...
. A retractable tailwheel was positioned just ahead of the tailplane leading edge. The first prototype, the VM-16, was crewed by just a pilot and navigator/gunner/bomb-aimer, seated alongside but facing rearwards. He remotely operated a calibre tail gun from this position but went into the semi-glazed nose for bombing. Development concentrated on increasing defensive armament. The ground-tested but unflown second prototype, the VM-17, added another crew member to operate its four guns. It was eventually modified into the Myasishchyev VB-109, described briefly below. The final prototype, the VM-18, had a 16% increase in span and 10% in length, with a fourth crew member in an extended rear cockpit to operate its guns, one in his cockpit and two more in remotely operated dorsal and ventral barbettes. There was also a forward firing gun. The VM-16 was first flown on 30 December 1944. The VM-17 was not flown until late 1945, after modification into the VB-109; the VM-18 was flown in 1946, though flight tests were not completed before programme cancellation.


Variants

Data from Russian Aircraft 1875-1995 ;VM-16: Two-seater. Single remotely operated calibre tail gun. First flown 30 December 1944. One only. ;VM-17: Three crew and extra armament. Empty weight increased by but dimensions unchanged. Ground-tested but unflown until converted into the VB-109. Four guns, three calibre, the other . One only. ;VM-18: Four crew, cockpit modified for gun. Span increased to and length to . Four guns, one fixed, forward firing and the others calibre, rearward firing. It was flown in 1946 but its tests were not completed when the programme was abandoned. One only. ;VB-109: Rebuilt two-seat VM-17, with the same span as the VM-16 and VM-17 and a length of . It had two seats in a pressurized cabin and was more heavily armour-plated than its predecessors. There were two guns, one remotely operated in the tail as in the VM-16 and another fixed. It was intended to have upgraded, two-stage supercharged
Klimov VK-109 The JSC Klimov (or Joint Stock Company Klimov) presently manufactures internationally certified gas turbine engines, main gearboxes and accessory drive gearboxes for transport aircraft. Originally established as ''Kirill Klimov Experimental De ...
engines, though interim
Klimov VK-107 The Klimov VK-107 was a V-12 liquid-cooled piston aircraft engine used by Soviet Union, Soviet aircraft during World War II. Development The VK-107 was developed from the Klimov M-105, M-105 and Klimov VK-106, VK-106. To achieve a greater power ...
As powered its first flight, made in late 1945. One only.


Specifications (VM-16)


See also


References

{{Myasishchev 1940s Soviet bomber aircraft World War II Soviet medium bombers Mid-wing aircraft Aircraft first flown in 1944 Twin piston-engined tractor aircraft DB-108