Thiokol solid rocket engine. In Production. Total flown included in total for Star-27E. Total impulse 88,555 kgf-sec. Motor propellant mass fraction 0.918.
AKA: TE-M-616-5. Status: In Production. Gross mass: 333 kg (734 lb). Unfuelled mass: 28 kg (61 lb). Specific impulse: 288 s. Diameter: 0.69 m (2.27 ft).