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RD-0255
Part of RD-0228 Family
RD-0255
RD-0255
Credit: KBKhA
Kosberg N2O4/UDMH rocket engine. R-36M2 / RS-20V (SS-18 Mod-4) stage 2. Comprises of single-chamber main engine RD-0256 plus four-chamber steering engines RD-0257. Development based on RD-0228 with thrust increase by 11%. First flight 1986.

Date: 1983-89. Number: 42 . Thrust: 755.00 kN (169,730 lbf).

Chambers: 1 + 4.



Family: Storable liquid. Country: Russia. Launch Vehicles: Dnepr. Propellants: N2O4/UDMH. Stages: R-36M2-2. Agency: Kosberg bureau. Bibliography: 309, 330, 342.

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