This page no longer updated from 31 October 2001.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-3. Used on launch vehicles: VLS. Gross Mass: 941 kg. Empty Mass: 127 kg. Propellants: Solid Thrust(vac): 33,900 kgf. Thrust(vac): 332.40 kN. Isp: 282 sec. Burn time: 68 sec. Diameter: 1.0 m. Length: 1.8 m. Chambers: 1. Chamber Pressure: 39.50 bar. Area Ratio: 66.00. Country: Brazil. Status: In Production. First Flight: 1997. Last Flight: 1997. Flown: 1.
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Last update 12 March 2001.
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© Mark Wade, 2001 .