Thiokol solid rocket engine. Out of Production. Total impulse 189,489 kgf-sec. Motor propellant mass fraction 0.91.
AKA: TE-M-364-2. Status: Out of Production. Number: 23 . Thrust: 45.00 kN (10,116 lbf). Gross mass: 718 kg (1,582 lb). Unfuelled mass: 64 kg (141 lb). Specific impulse: 291 s. Diameter: 0.93 m (3.07 ft).