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
R-56 Blok B
Notional Nitric acid/Kerosene rocket engine. R-56 Blok B. Notional engines for polyblock R-56, immense booster/ICBM; planned range 16,000 km. payload 35,000 kg. TsNIIMash has 1:10 structural simulation model.

Date: 1961. Thrust: 784.00 kN (176,250 lbf). Specific impulse: 330 s. Burn time: 205 s.

Propellant Formulation: RFNA/Kerosene.



Family: Storable liquid. Country: Russia. Launch Vehicles: R-56. Propellants: Nitric acid/Kerosene. Stages: R-56 Polyblock Stage B, R-56 Block B. Bibliography: 194.

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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use