This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Designer: Instituto de Aeronautica e Espaco. Used on stages: VLS-0. Used on launch vehicles: VLS. Gross Mass: 8,425 kg. Empty Mass: 1,245 kg. Propellants: Solid Thrust(vac): 309,000 kgf. Thrust(vac): 3,030.20 kN. Isp: 265 sec. Isp (sea level): 225 sec. Burn time: 59 sec. Diameter: 1.0 m. Length: 9.0 m. Chambers: 1. Chamber Pressure: 56.20 bar. Area Ratio: 12.82. Country: Brazil. Status: In Production. First Flight: 1997. Last Flight: 1997. Flown: 4.
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Last update 12 March 2001.
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© Mark Wade, 2001 .