In the engine compressor regulation introduced by restart air for the first stage. The engine has axial eight-stage compressor with subsonic high-pressure stages. Apply on-board automatic launching of turbine starter C-300M through fluid flywheel. The engine and its modifications set at TU-16, F-4, Tu-104.

The engine from domestic and foreign turbo-jet engines differs lowest (more than half as much) specific thrust (0.0227 kg / N). At this engine for the first time in domestic practice, used an electric starter - a generator. The engine used on the Yak-25.

At the engine for the first time in domestic practice, installed the supersonic first stage compressor and used fuel - oil aggregate.

When designing the engine widely used engine experience knot finishing AM-5. The engine has nine-stage axial compressor, cannular combustion chamber, two-stage turbine, afterburner, three-position nozzle

At the engine used double-speed drive starter - generator, and used carburetor ignition afterburner.

In the engine for the first time used: twin-shaft rotor scheme, construction rotors without remote pier, fuelling an igniter with oxygen, the first time developed a twin-shaft engine regulatory principles in a wide range of flight speeds. The engine has the most massive used on aircraft MiG-21 family.

The engine is a compact, has light weight, and its easy to manufacture.

The cheap and reliable engine for installation on training and sports aircraft Yak-30 and Yak-32. At the engine used seven-stage axial compressor, annular combustion chamber, single-stage turbine and unregulated jet nozzle. Modifying the engine RU19A - 300 applied as an auxiliary engine on civilian airplanes An - 24 and its modifications An - 26 and An-30. The engine is technological, has a great resource.

The single-shaft turbofan engine. The engine has electronic automatic control system, built an electric generator capacity of 4 kW and autonomous oil system. The engine capable of screening air for aircraft.

The turbofan engine with afterburner, with the opposite direction of rotation of rotors, with heightened gas-dynamic resistance compressors, with unique vortex burners in the main combustion chamber. For the engine developed the new turning nozzle with adjustable area nozzle throat, adjustable vectored thrust in the vertical plane on the range of 95 deg. regardless of engine regime. The engine was installed at Yak-141 on which it was established 12 world records.

The twin-shaft engine, has curvilinear nozzle with two pivoting restrictions nozzles which are listed in the motion of two hydraulic motors with sprung sync. The engine is highly gas-dynamic resistant, even in extreme conditions with the level of uneven temperatures and pulsations pressure air inlet. The engine was installed at Yak-38.

The single-shaft turbojet engine has five-stage axial compressor, input guide apparatus, cannular combustion chamber, single-stage turbine, afterburner, three-position nozzleб automatic launching of turbine starter C-300M. For the first time duration of the flight was secured at afterburning mode. At the engine for the first time in the world has been applied electronic control regimes. Engine modifications: R15K - 300, R15BF - 300, R15BF2 - 300. On planes with engines family R15B - 300 reached more than 30 world records of speed, altitude and rate. Implemented by plane MiG-25 and its modifications.