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.