3Д81 supersonic ramjet used in P-270 Moskit cruise missile system, designed by Designer General I.S. Seleznev. This engine realizes the concept of solid-propellant booster being within scramjet combustion chamber. This booster is ejected after finishing its working by ram air.



31ДП scramjet for Kh-31A and Kh-31P cruise missiles, produced by JSC Tactical Missiles Corporation. Genuine control and regulation system of working process provide engine’s working life in extensive altitude and velocity envelope. Such systems have no counterparts in the world.


Dual-component liquid rocket engines with thrust from 0,04 to 40 kgf, installed on 9 different power plants, designed by Turaevo Machine-building Design Bureau “SOYUZ” for space vehicles, created under  the direction of such Chief managers as, S.P. Korolev, V.P. Mishin, G.N. Babakin, I.F. Reshetnev, V.N. Chelomey, and G.Ye.Lozino-Lozinskiy. 11Д444 liquid rocket engine with thrust from 40 gram, currently has no counterparts, running on duel-component fuel.