8D725

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8D725

Part of RD-280

Glushko N2O4/UDMH rocket engine. Developed 1963-1970. 10 to 12 metric ton thrust engine developed for an unstated military requirement.

Status: Developed 1963-1970. Date: 1963-1970. Thrust: 117.00 kN (26,302 lbf). Specific impulse: 325 s.

Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. Agency: Glushko bureau. Bibliography: 283.

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