Star 37X
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Thiokol solid rocket engine. Out of Production. Total impulse 310,668 kgf-sec. Motor propellant mass fraction 0.928.
Thrust (sl): 39.600 kN (8,902 lbf). Thrust (sl): 4,039 kgf.