S-40TM (original) (raw)

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S-40TM

IAE solid rocket engine. Used on VLS launch vehicle. First flight 1985.

Status: Active. Number: 5 . Thrust: 208.40 kN (46,850 lbf). Gross mass: 5,359 kg (11,814 lb). Unfuelled mass: 929 kg (2,048 lb). Specific impulse: 272 s. Specific impulse sea level: 204 s. Burn time: 56 s. Height: 5.80 m (19.00 ft). Diameter: 1.00 m (3.20 ft).

Thrust (sl): 155.000 kN (34,845 lbf). Thrust (sl): 15,764 kgf. Chamber Pressure: 57.20 bar. Area Ratio: 25.97.

Country: Brazil. Launch Vehicles: VLS, VLS-R1, VLS-1, VLM, VS-40. Propellants: Solid. Stages: S-40TM. Agency: IAE.

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