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Engine Model: S-30. Designer: IAE. Gross Mass: 377 kg (831 lb). Empty Mass: 57 kg (125 lb). Propellants: Solid. Thrust(vac): 20.490 kN (4,606 lbf). Isp: 275 sec. Burn time: 43 sec. Diameter: 0.66 m (2.16 ft). Length: 1.25 m (4.10 ft). Chambers: 1. Country: Brazil. Status: Development ended 1997.
S-30 used on Rocket Stages
- Used on stage: VLM-4. on launch vehicle: VLS.
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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