SLV-1 Designer: ISRO. Gross Mass: 10,800 kg (23,800 lb). Empty Mass: 2,140 kg (4,710 lb). Propellants: Solid. Thrust(vac): 502.600 kN (112,989 lbf). Thrust(sl): 454.900 kN (102,266 lbf). Isp: 253 sec. Isp (sea level): 229 sec. Burn time: 49 sec. Diameter: 1.00 m (3.20 ft). Length: 9.99 m (32.77 ft). Chambers: 1. Chamber Pressure: 43.00 bar. Area Ratio: 6.70. Country: India. First Flight: 1979. Last Flight: 2003. Flown: 64. SLV-1 used on Rocket Stages Used on stage: ASLV-0. on launch vehicle: ASLV. Used on stage: ASLV-1. on launch vehicle: ASLV. Used on stage: PSLV-0. on launch vehicle: PSLV. Used on stage: SLV-1. on launch vehicle: SLV.                   Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2007 except where otherwise noted.

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