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Star 37E
Part of Star 37
Thiokol solid rocket engine. Out of Production. Total impulse 296,635 kgf-sec. Motor propellant mass fraction 0.926.

AKA: TE-M-364-4. Status: Out of Production. Number: 91 . Thrust: 68.00 kN (15,287 lbf). Gross mass: 1,123 kg (2,475 lb). Unfuelled mass: 83 kg (182 lb). Specific impulse: 284 s. Burn time: 42 s. Diameter: 0.93 m (3.07 ft).

Country: USA. Launch Vehicles: Atlas F/PTS, Atlas F/SVS, N-2, Atlas E/SVS, Delta 3924. Propellants: Solid. Stages: Star 37E. Agency: Thiokol. Bibliography: 410.
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