This page no longer updated from 31 October 2001. Latest version can be found at A-6

Redstone engine
Redstone engine -

Credit: © Mark Wade. 10,228 bytes. 386 x 305 pixels.

Designer: Rocketdyne. Used on stages: Redstone. Used on launch vehicles: Redstone. Propellants: Lox/Alcohol Thrust(vac): 42,251 kgf. Thrust(vac): 414.30 kN. Isp: 265 sec. Isp (sea level): 235 sec. Burn time: 155 sec. Mass Engine: 658 kg. Diameter: 1.8 m. Chambers: 1. Country: USA. Status: Out of Production. First Flight: 1960. Last Flight: 1967. Flown: 16.
Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .