Redstone Redstone engine Credit - © Mark Wade Gross Mass: 28,440 kg (62,690 lb). Empty Mass: 3,125 kg (6,889 lb). Thrust (vac): 414.340 kN (93,147 lbf). Isp: 265 sec. Burn time: 155 sec. Propellants: Lox/Alcohol. Isp(sl): 235 sec. Diameter: 1.77 m (5.80 ft). Span: 4.19 m (13.74 ft). Length: 17.58 m (57.67 ft). Country: USA. No Engines: 1. Engine: A-6. Status: Out of production. Cost $ : 4.930 million. First Flight: 1953. Last Flight: 1967. No Launched: 148. Used on Launch Vehicles: Redstone.                   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 - 2007 except where otherwise noted.

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