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Engine Model: SLV-2. Designer: ISRO. Gross Mass: 4,900 kg (10,800 lb). Empty Mass: 1,750 kg (3,850 lb). Propellants: Solid. Thrust(vac): 267.000 kN (60,023 lbf). Thrust(sl): 216.000 kN (48,558 lbf). Isp: 267 sec. Isp (sea level): 216 sec. Burn time: 40 sec. Diameter: 0.80 m (2.62 ft). Length: 6.35 m (20.83 ft). Chambers: 1. Chamber Pressure: 43.00 bar. Area Ratio: 14.00. Country: India. First Flight: 1979. Last Flight: 1994. Flown: 8.00.
SLV-2 used on Rocket Stages - Used on stage: SLV-2. on launch vehicle: ASLV.
- Used on stage: SLV-2. on launch vehicle: SLV.
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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