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Algol 3A

Engine · USA

Original archive entry. The text, images and links below are kept as they were written.

CSD solid rocket engine. In Production.

Thrust (sl): 405.500 kN (91,160 lbf). Thrust (sl): 41,349 kgf. Chamber Pressure: 31.00 bar. Area Ratio: 6.5.

Country
USA
Launch Vehicles
Scout D-1 F, Scout E-1
Propellants
Solid
Stages
Algol 3A
Agency
CSD