RD-0213

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Engine Model: RD-0213. Manufacturer Name: RD-0213. Government Designation: 8D48. Other Designations: RD-473. Designer: Kosberg. Developed in: 1962-68. Application: Proton stage 3. Propellants: N2O4/UDMH. Thrust(vac): 582.100 kN (130,861 lbf). Thrust(sl): 446.000 kN (100,264 lbf). Isp: 327 sec. Burn time: 230 sec. Diameter: 4.15 m (13.61 ft). Chambers: 4. Chamber Pressure: 147.00 bar. Area Ratio: 81.30. Country: Russia. Status: Design 1962.

Version of RD-0210. Staged combustion cycle (Oxidizer pre-burner gas routed to main chamber after driving turbine). Main engine for Proton Stage 3 in system RD-0212.

RD-0213 used on Rocket Stages

Used on stage: Proton-2. on launch vehicle: Proton.

Used on stage: Proton-2. on launch vehicle: UR-200.

Used on stage: R-56 Block O. on launch vehicle: R-56.

Bibliography:

Haeseler, Dietrich, Visit to the museum of Chemical Automatics Design Bureau, Voronezh 1992 via Dietrich Haeseler.

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