This page no longer updated from 31 October 2001. Latest version can be found at Algol 2

Designer: United Technologies. Used on stages: Algol 2. Used on launch vehicles: Scout A, Scout B, Scout X-3, Scout X-4, Titan 3BAS2. Gross Mass: 11,600 kg. Empty Mass: 1,650 kg. Propellants: Solid Thrust(vac): 57,537 kgf. Thrust(vac): 564.20 kN. Isp: 255 sec. Isp (sea level): 232 sec. Burn time: 47 sec. Diameter: 1.0 m. Length: 9.1 m. Chambers: 1. Country: USA. Status: Out of Production. First Flight: 1962. Last Flight: 1976. Flown: 67.
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 .