Thiokol solid rocket engine. Out of Production. Total impulse 275,959 kgf-sec. Motor propellant mass fraction 0.921.
AKA: TE-M-364-18. Status: Out of Production. Number: 9 . Thrust: 45.00 kN (10,116 lbf). Gross mass: 1,048 kg (2,310 lb). Unfuelled mass: 83 kg (182 lb). Specific impulse: 286 s. Diameter: 0.93 m (3.07 ft).