Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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-851
Yuzhnoye Nitric acid/UDMH rocket engine. R-16 (SS-7) stage 1 attitude control engine . Out of Production. Four thrusters are each gimbaled in one single axis.

AKA: 8D63. Status: Out of Production. Date: 1958-63. Thrust: 32.48 kN (7,302 lbf). Unfuelled mass: 403 kg (888 lb). Specific impulse: 279 s. Specific impulse sea level: 243 s. Burn time: 115 s. Height: 1.70 m (5.50 ft). Diameter: 3.54 m (11.61 ft).

Chambers: 4. Engine: 403 kg (888 lb). Chamber Pressure: 66.20 bar. Propellant Formulation: AK27/UDMH. Thrust to Weight Ratio: 8.21. Oxidizer to Fuel Ratio: 2.45.

Subtopics
RD-852 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.
Family: Storable liquid. Country: Ukraine. Launch Vehicles: R-16. Propellants: Nitric acid/UDMH. Agency: Yuzhnoye. Bibliography: 344, 348.
Back to top of page
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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
© 1997-2019 Mark Wade - Contact
© / Conditions for Use