Thiokol solid rocket engine. In Production. Total flown included in total for Star-27E. Total impulse 88,668 kgf-sec. Motor propellant mass fraction 0.921.
AKA: TE-M-616-8. Status: In Production. Gross mass: 332 kg (731 lb). Unfuelled mass: 26 kg (57 lb). Specific impulse: 288 s. Diameter: 0.69 m (2.27 ft).