Thiokol solid rocket engine. Out of Production. Total impulse 249,177 kgf-sec. Motor propellant mass fraction 0.928.
AKA: TE-M-364-19. Status: Out of Production. Number: 19 . Thrust: 55.50 kN (12,477 lbf). Gross mass: 934 kg (2,059 lb). Unfuelled mass: 67 kg (147 lb). Specific impulse: 286 s. Burn time: 42 s. Diameter: 0.93 m (3.07 ft).