Star 48A s
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Credit: Thiokol
Thiokol solid rocket engine. In Production. Short nozzle upper-stage motor designed to fit within the dimensional envelope of the long nozzle.
Total flown included in total for Star-48A-l. Total impulse 693,030 kgf-sec. Motor propellant mass fraction 0.944.