RD-0234
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
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.
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.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- N2O4/UDMH
- Stages
- UR-100N Stage 1N
- Agency
- Kosberg bureau