Thiokol solid rocket engine. In Production. Total flown included in total for Star-27E. Total impulse 89,684 kgf-sec. Motor propellant mass fraction 0.919.
AKA: TE-M-616-1. Status: In Production. Gross mass: 336 kg (740 lb). Unfuelled mass: 27 kg (59 lb). Specific impulse: 288 s. Diameter: 0.69 m (2.27 ft).