R-56 Blok A (original) (raw)

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R-56 Blok A

Notional Nitric acid/Kerosene rocket engine. R-56 Blok A. 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: 4,412.00 kN (991,857 lbf). Specific impulse: 320 s. Specific impulse sea level: 300 s. Burn time: 142 s.

Propellant Formulation: RFNA/Kerosene.

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

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