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RD-852


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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-852 Part of RD-851 Yuzhnoye Nitric acid/UDMH rocket engine. R-16 (SS-7) stage 2 attitude control engine. Out of Production. Four thrusters are each gimbaled in one single axis.

Status: Out of Production. Date: 1958-63. Thrust: 48.25 kN (10,847 lbf). Unfuelled mass: 133 kg (293 lb). Specific impulse: 255 s. Burn time: 143 s. Height: 2.40 m (7.80 ft). Diameter: 2.95 m (9.67 ft).

Chambers: 4. Engine: 133 kg (293 lb). Chamber Pressure: 66.20 bar. Propellant Formulation: AK27/UDMH. Thrust to Weight Ratio: 36.99. Oxidizer to Fuel Ratio: 2.4.

Family: Storable liquid. Country: Ukraine. Launch Vehicles: R-16. Propellants: Nitric acid/UDMH. Agency: Yuzhnoye. Bibliography: 348. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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