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RD-0206


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A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z RD-0206 Part of RD-0202 Kosberg N2O4/UDMH rocket engine. UR-200 stage 2. Developed 1961-64. Staged combustion cycle. First flight 1964.

AKA: 8D47. Status: Developed 1961-64. Date: 1961-64. Thrust: 575.50 kN (129,378 lbf). Specific impulse: 326 s. Burn time: 150 s. Diameter: 1.47 m (4.82 ft).

Chamber Pressure: 147.00 bar. Area Ratio: 81.3. Oxidizer to Fuel Ratio: 2.6.

Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. Stages: UR-200-2. Agency: Kosberg bureau. Bibliography: 309, 320, 7475. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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