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RD-0200


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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-0200 Kosberg Nitric acid/Amine rocket engine. Lavochkin SAM, flew 1960. Out of Production. First liquid rocket engine by OKB-154, evolution of Isayev S2.1200 transferred to Kosberg. Thrust range 59 - 5.9 kN. Sea level specific impulse 230 - 166 sec

AKA: RO1-154. Status: Out of Production. Date: 1957-62. Thrust: 58.80 kN (13,219 lbf). Unfuelled mass: 86 kg (189 lb). Specific impulse: 230 s. Specific impulse sea level: 230 s. Burn time: 360 s. Height: 0.40 m (1.31 ft). Diameter: 0.30 m (0.98 ft).

Chambers: 2. Throttled thrust(vac): 5.900 kN (1,326 lbf). Engine: 86 kg (189 lb). Chamber Pressure: 66.00 bar. Propellant Formulation: AK27I/TG-02. Thrust to Weight Ratio: 69.72.

Subtopics R-101B.36000-0 Isayev Nitric acid/Amine rocket engine. Single chamber engine designed for use in the R-101B and R-108 (derivative of German Wasserfall). RD-0201 Kosberg Nitric acid/Amine rocket engine. SAM V1100 by Grushin stage 3. Out of Production. Thrust range 59 - 28 kN. First flight 1960. Family: Storable liquid. Country: Russia. Propellants: Nitric acid/Amine. Agency: Kosberg bureau. Bibliography: 307, 342, 95. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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