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Engine Model: SLV-4. Designer: ISRO. Gross Mass: 360 kg (790 lb). Empty Mass: 98 kg (216 lb). Propellants: Solid. Thrust(vac): 26.800 kN (6,025 lbf). Thrust(sl): 5.690 kN (1,279 lbf). Isp: 283 sec. Isp (sea level): 60 sec. Burn time: 33 sec. Diameter: 0.66 m (2.16 ft). Length: 1.50 m (4.90 ft). Chambers: 1. Chamber Pressure: 29.00 bar. Area Ratio: 31.00. Country: India. First Flight: 1979. Last Flight: 1994. Flown: 8.00.
SLV-4 used on Rocket Stages - Used on stage: SLV-4. on launch vehicle: ASLV.
- Used on stage: SLV-4. on launch vehicle: SLV.
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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