Agni-1

home topic index

Model: Agni 2-1. Gross Mass: 11,500 kg (25,300 lb). Empty Mass: 2,900 kg (6,300 lb). Thrust (vac): 700.000 kN (157,360 lbf). Burn time: 50 sec. Propellants: Solid. Diameter: 1.00 m (3.20 ft). Length: 11.00 m (36.00 ft). Country: India. No Engines: 1. Motor: Agni. Status: Active. First Flight: 1989. Last Flight: 2007. No Launched: 11. Used as: ASLV. Release conditions: DRDO. Model: Agni 3-1. Gross Mass: 33,000 kg (72,000 lb). Empty Mass: 2,970 kg (6,540 lb). Thrust (vac): 1,040.000 kN (233,800 lbf). Burn time: 75 sec. Propellants: Solid. Diameter: 2.00 m (6.50 ft). Length: 7.70 m (25.20 ft). Country: India. No Engines: 1. Motor: Agni3. 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.