Encyclopedia Astronautica
Agni 2-2


Solid propellant rocket stage. Loaded mass 4,200 kg.

Status: Active.
Gross mass: 4,200 kg (9,200 lb).
Height: 6.00 m (19.60 ft).
Diameter: 1.00 m (3.20 ft).
Burn time: 60 s.
Number: 3 .

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...

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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