Kholshchevnikov VRDK


The Kholshchevnikov VRDK ', or E-3020''', was a motorjet developed in the Soviet Union during World War II. The VRDK was designed to give fighter aircraft a ten-minute performance boost during combat.
VRDK boosters were built in small numbers for use in the Mikoyan-Gurevich I-250 and Sukhoi Su-5 mixed propulsion fighter aircraft. Both aircraft made their first flights in 1945, shortly before the end of World War II.
Interest in VRDK technology declined quickly after World War II as Soviet designers focused on the development of turbojet powered fighter aircraft.

Design and development

Design work on VRDK technology started in 1941 at the Central Aerohydrodynamic Institute with the goal of developing a motorjet where a piston engine would be combined with an axial flow compressor. From 1943 work was handed over to the Baranov Central [Institute of Aviation Motor Development|Central Institute of Aviation Motors] where design studies separated into two branches. One branch of research headed by A.I Tolstov focused on diesel engines the other headed by Professor K.V Kholshchevnikov focused on spark ignition engines.
In May 1944 the GKO ordered the major aircraft design bureaus to start developing aircraft that used a piston engine as their primary powerplant augmented with a small rocket or jet engine booster for short bursts of speed. The Mikoyan-Gurevich and Sukhoi design bureaus opted to use the VRDK developed by Kholshchevnikov's team which was formally known as the E-3020 while being informally known as the Kholshchevnikov accelerator.
Both the Sukhoi Su-5 and Mikoyan-Gurevich I-250 used a single Klimov VK-107 engine to drive a propeller and the VRDK’s single stage axial flow compressor. The VRDK was driven from a step-up gearbox and could be engaged/disengaged by the pilot via a clutch mechanism which connected it to the piston engine via a shaft. Air supplied by a duct running from the front of the aircraft was mixed with engine exhaust then compressed and fed to an afterburner before exiting via a nozzle at the back of the aircraft. Part of the compressor exhaust was also used to supercharge the engine. To protect the pilot and airframe, the VRDK was cooled during operation by water from a tank mounted in the fuselage.
When tested in the I-250, the thrust from the VRDK was and combined output from the piston engine + VRDK was calculated to be the equivalent of.
The VRDK was designed to operate for 10 minutes continuously and provide a speed increase of. Both the Su-5 and the I-250 had top speeds faster than contemporary piston engined fighters but slower than early jet fighters such as the Gloster Meteor and Messerschmitt Me 262.
Only small numbers of Soviet motorjet aircraft were built and none saw service during World War II. After the war interest in motorjets quickly declined as the Soviets acquired German and British turbojet engines. Research, development and flight testing of Soviet motorjet aircraft had finished by 1950.

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