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S-40TM
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Designer: Instituto de Aeronautica e Espaco. Gross Mass: 5,359 kg (11,814 lb). Empty Mass: 929 kg (2,048 lb). Propellants: Solid. Thrust(vac): 208.400 kN (46,850 lbf). Thrust(sl): 155.000 kN (34,845 lbf). Isp: 272 sec. Isp (sea level): 204 sec. Burn time: 56 sec. Diameter: 1.00 m (3.20 ft). Length: 5.80 m (19.00 ft). Chambers: 1. Chamber Pressure: 57.20 bar. Area Ratio: 25.97. Country: Brazil. First Flight: 1985. Last Flight: 2003. Flown: 5.00.
S-40TM used on Rocket Stages - Used on stage: VLS-2. on launch vehicle: VLM.
- Used on stage: VLS-2. on launch vehicle: VLS.
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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