Thiokol solid rocket engine. Out of Production. Total impulse 162,102 kgf-sec. Motor propellant mass fraction 0.898.
AKA: TE-M-364-14. Status: Out of Production. Number: 9 . Thrust: 45.00 kN (10,116 lbf). Gross mass: 623 kg (1,373 lb). Unfuelled mass: 64 kg (141 lb). Specific impulse: 290 s. Diameter: 0.93 m (3.07 ft).