This page no longer updated from 31 October 2001.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-1. Used on launch vehicles: VLS. Gross Mass: 8,404 kg. Empty Mass: 1,224 kg. Propellants: Solid Thrust(vac): 327,000 kgf. Thrust(vac): 3,206.70 kN. Isp: 276 sec. Isp (sea level): 170 sec. Burn time: 58 sec. Diameter: 1.0 m. Length: 8.1 m. Chambers: 1. Chamber Pressure: 55.30 bar. Area Ratio: 37.68. 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 .