Proton 11S824F

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Proton 11S824F

Part of Block D

LOx/Kerosene propellant rocket stage. Also known as Block D-2; article number 11S824F. Without guidance unit (navigation commands come from payload). Successor to 11S824M. Used for launch of Lavochkin Mars-bound spacecraft in 1988 and 1996.

AKA: 11S824;11S824F;Block D;D-1-e. Status: Retired 1996. Thrust: 85.02 kN (19,113 lbf). Gross mass: 16,900 kg (37,200 lb). Unfuelled mass: 1,800 kg (3,900 lb). Specific impulse: 352 s. Burn time: 610 s. Height: 5.50 m (18.00 ft). Diameter: 3.70 m (12.10 ft). Span: 3.70 m (12.10 ft).

Cost $ : 4.000 million.

Family: Space Tugs. Country: Russia. Engines: RD-58M, 11D79. Launch Vehicles: Proton-K/D-2. Propellants: Lox/Kerosene.

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