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Star 24C

Engine · USA

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

Star-24C
Star-24C
Credit: Thiokol

Thiokol solid rocket engine. In Production. Apogee motor designed and qualified for the NASA International Ultraviolet Experiment satellite.

It incorporates a 1.5-inch longer cylindrical section with increased propellant weight and a larger nozzle throat and operates at a slightly higher chamber pressure than prior STAR 24 motors. Total impulse 62,573 kgf-s. Propellant mass fraction 0.917.

Country
USA
Propellants
Solid
Agency
Thiokol
Bibliography
410