Agni-2

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Model: Agni 2-2. Gross Mass: 4,200 kg (9,200 lb). Burn time: 60 sec. Propellants: Solid. Diameter: 1.00 m (3.20 ft). Length: 6.00 m (19.60 ft). Country: India. No Engines: 1. Motor: Agni St2. Status: Active. First Flight: 1999. Last Flight: 2004. No Launched: 3. Used as: Agni II Stage 2. Release conditions: DRDO. Model: Agni 3-2. Gross Mass: 14,000 kg (30,000 lb). Empty Mass: 1,820 kg (4,010 lb). Thrust (vac): 314.000 kN (70,590 lbf). Burn time: 110 sec. Propellants: Solid. Diameter: 2.00 m (6.50 ft). Length: 3.10 m (10.10 ft). Country: India. No Engines: 1. Motor: Agni3 S2. Status: Active. First Flight: 2006. Last Flight: 2007. No Launched: 2. Used as: Agni3. Release conditions: DRDO. Used on Launch Vehicles: Agni. 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 - 2008 except where otherwise noted.