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RD-225
Glushko Nitric acid/UDMH rocket engine. R-26 stage 1. Out of Production. Two clustered together to make RD-224. First flight 1961.

Status: Out of Production. Date: 1960-62. Thrust: 889.00 kN (199,855 lbf). Specific impulse: 294 s. Specific impulse sea level: 251 s. Burn time: 100 s.

Chambers: 2. Chamber Pressure: 83.40 bar. Area Ratio: 21. Propellant Formulation: AK27P/UDMH. Oxidizer to Fuel Ratio: 2.5.

Subtopics
RD-224 Glushko Nitric acid/UDMH rocket engine. R-26 stage 1. Out of production. RD-224 is a block of 2 RD-225s. An upper stage thrust chamber was developed under designation U102-000. First flight 1961.
Family: Storable liquid. Country: Russia. Propellants: Nitric acid/UDMH. Agency: Glushko bureau. Bibliography: 320.
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