Encyclopedia Astronautica
Agni 2-1


Solid rocket stage. 700.00 kN (157,366 lbf) thrust. Mass 11,500 kg (25,353 lb).

Status: Active.
Gross mass: 11,500 kg (25,300 lb).
Unfuelled mass: 2,900 kg (6,300 lb).
Height: 11.00 m (36.00 ft).
Diameter: 1.00 m (3.20 ft).
Thrust: 700.00 kN (157,360 lbf).
Burn time: 50 s.
Number: 11 .

More... - Chronology...


Associated Countries
Associated Engines
Associated Launch Vehicles
  • Agni 2 Indian intermediate range ballistic missile. Program revived in 1998, assumed to be nuclear warhead-capable. More...
  • Agni 1 Indian single-stage short range ballistic missile. More...

Associated Manufacturers and Agencies
  • DRDO Indian manufacturer of rocket engines. DRDO, India. More...

Associated Propellants
  • Solid Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. More...

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