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Star 6
Thiokol solid rocket engine. Out of Production. Total flown included in total for Star-6A. Total impulse 1,395 kgf-sec. Motor propellant mass fraction 0.795.

AKA: TE-M-541-3. Status: Out of Production. Gross mass: 6.11 kg (13.47 lb). Unfuelled mass: 1.25 kg (2.75 lb). Specific impulse: 287 s. Diameter: 0.16 m (0.52 ft).



Subtopics

Star 6A Thiokol solid rocket engine. Out of Production. Total impulse 935 kgf-sec. Motor propellant mass fraction 0.723.

Star 6B Thiokol solid rocket engine. In Production. Delta-V reentry motor developed as a spin-up and propulsion motor for reentry vehicles. The design incorporated an aluminum case and a plastic nozzle assembly.

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

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