Thiokol solid rocket engine. Out of Production. Total impulse 190,590 kgf-sec. Motor propellant mass fraction 0.925.
AKA: TE-M-364-15. Status: Out of Production. Number: 20 . Thrust: 45.00 kN (10,116 lbf). Gross mass: 711 kg (1,567 lb). Unfuelled mass: 53 kg (116 lb). Specific impulse: 287 s. Diameter: 0.93 m (3.07 ft).