S-43TM (original) (raw)

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S-43TM

Part of S-43

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

Status: Active. Number: 5 . Thrust: 321.70 kN (72,321 lbf). Gross mass: 8,404 kg (18,527 lb). Unfuelled mass: 1,224 kg (2,698 lb). Specific impulse: 276 s. Specific impulse sea level: 170 s. Burn time: 58 s. Height: 8.10 m (26.50 ft). Diameter: 1.00 m (3.20 ft).

Thrust (sl): 197.000 kN (44,287 lbf). Thrust (sl): 20,069 kgf. Chamber Pressure: 55.30 bar. Area Ratio: 37.68.

Country: Brazil. Launch Vehicles: VLS, VLS-R1, VLS-1, VLM. Propellants: Solid. Stages: S-43TM. Agency: IAE.

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