SLS SRB 388

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SLS SRB 388

Solid propellant rocket stage. Booster for SLS A series launch vehicles.

Status: Study 1961. Thrust: 2,083.90 kN (468,479 lbf). Gross mass: 88,000 kg (194,000 lb). Unfuelled mass: 13,000 kg (28,000 lb). Specific impulse: 260 s. Specific impulse sea level: 235 s. Burn time: 90 s. Height: 16.40 m (53.80 ft). Diameter: 2.58 m (8.46 ft). Span: 2.58 m (8.46 ft).

Country: USA. Launch Vehicles: SLS A-410, SLS A-388. Propellants: Solid.

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