PRD-33

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Engine Model: PRD-33. Designer: SKB-30. Gross Mass: 3,000 kg (6,600 lb). Propellants: Solid. Thrust(vac): 1,962.000 kN (441,075 lbf). Burn time: 4.50 sec. Diameter: 1.00 m (3.20 ft). Length: 3.10 m (10.10 ft). Country: Russia. PRD-33 used on Rocket Stages Used on stage: V-1000. on launch vehicle: V-1000. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.