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RD-254
Part of RD-253 Family
Glushko N2O4/UDMH rocket engine. N-1 upper stage, UR-700 stage 3. Proposed for use in N-1. High altitude version of RD-253 for 2nd stages. Later proposed for R-56 and UR-700 upper stages.

Status: Study 1961. Date: 1962-66. Thrust: 1,716.00 kN (385,772 lbf).



Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. Stages: R-56 Block B, UR-700-3. Agency: Glushko bureau. Bibliography: 323.

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