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Star 30A
Part of Star 30
Thiokol solid rocket engine. Out of Production. Total impulse 137,095 kgf-sec. Motor propellant mass fraction 0.942.

AKA: TE-M-700-4. Status: Out of Production. Number: 4 . Gross mass: 492 kg (1,084 lb). Unfuelled mass: 28 kg (61 lb). Specific impulse: 295 s. Diameter: 0.76 m (2.50 ft).

Country: USA. Propellants: Solid. Agency: Thiokol. Bibliography: 410.
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