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RD-0234
Kosberg N2O4/UDMH rocket engine. UR-100N / RS-18 (SS-19) stage 1. Out of Production. Staged combustion cycle. Modification of RD-0233 including tank pressurization system. First flight 1974.

Status: Out of Production. Date: 1969-74. Thrust: 520.00 kN (116,900 lbf). Specific impulse: 310 s. Specific impulse sea level: 285 s. Burn time: 121 s.

Chamber Pressure: 205.00 bar.



Subtopics

RD-0233 Kosberg N2O4/UDMH rocket engine. UR-100N / RS-18 (SS-19) stage 1. Out of Production. Staged combustion cycle. First flight 1974.

RD-0234-CH Kosberg LOx/LCH4 rocket engine. Developed 1996-. Proposed variant of RD-0234 engine using LOX-liquid methane instead of N2O4/UDMH as propellants.

RD-0234-HC Kosberg LOx/Kerosene rocket engine. Developed 1996-. Proposed variant of RD-0234 engine using LOX-kerosene instead of N2O4/UDMH as propellants.

Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. Stages: UR-100N Stage 1N. Agency: Kosberg bureau. Bibliography: 309, 339, 342, 353, 7487.

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