S-30 engine (original) (raw)

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S-30 engine

Part of S-30

IAE solid rocket engine. Development ended 1997. VLM fourth stage.

AKA: S-30;VLM-4. Status: Development ended 1997. Thrust: 20.49 kN (4,606 lbf). Gross mass: 377 kg (831 lb). Unfuelled mass: 57 kg (125 lb). Specific impulse: 275 s. Burn time: 43 s. Height: 1.25 m (4.10 ft). Diameter: 0.66 m (2.16 ft).

Propellant Formulation: HTPB.

Country: Brazil. Launch Vehicles: Sonda 3, Sonda 3 M1, Sonda 4, VS-30, VLM, VS-30/Orion, VSB-30. Propellants: Solid. Stages: S-30 engine. Agency: IAE.

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