Encyclopedia Astronautica
Agni3 S2


DRDO solid rocket engine. 314 kN.

Gross mass: 14,000 kg (30,000 lb).
Unfuelled mass: 1,820 kg (4,010 lb).
Height: 3.10 m (10.10 ft).
Diameter: 2.00 m (6.50 ft).
Thrust: 314.00 kN (70,590 lbf).
Burn time: 110 s.

More... - Chronology...


Associated Countries
See also
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...

Associated Stages
  • Agni 3-2 Solid rocket stage. 314.00 kN (70,590 lbf) thrust. Mass 14,000 kg (30,865 lb). More...

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