Thiokol solid rocket engine. Out of Production. Total flown included in total for Star-37XF-8. Total impulse 259,123 kgf-sec. Motor propellant mass fraction 0.929.
AKA: TE-M-714-6. Status: Out of Production. Thrust: 45.00 kN (10,116 lbf). Gross mass: 953 kg (2,101 lb). Unfuelled mass: 68 kg (149 lb). Specific impulse: 290 s. Diameter: 0.93 m (3.06 ft).