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Engine Model: SLV-3. Designer: ISRO. Gross Mass: 1,500 kg (3,300 lb). Empty Mass: 440 kg (970 lb). Propellants: Solid. Thrust(vac): 90.700 kN (20,390 lbf). Thrust(sl): 62.200 kN (13,983 lbf). Isp: 277 sec. Isp (sea level): 190 sec. Burn time: 45 sec. Diameter: 0.82 m (2.69 ft). Length: 2.30 m (7.50 ft). Chambers: 1. Chamber Pressure: 43.00 bar. Area Ratio: 24.00. Country: India. First Flight: 1979. Last Flight: 1994. Flown: 8.00.
SLV-3 used on Rocket Stages - Used on stage: SLV-3. on launch vehicle: ASLV.
- Used on stage: SLV-3. on launch vehicle: SLV.
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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