Encyclopedia Astronautica
Agni 3-1


Solid rocket stage. 1040.00 kN (233,801 lbf) thrust. Mass 33,000 kg (72,753 lb).

Status: Active.
Gross mass: 33,000 kg (72,000 lb).
Unfuelled mass: 2,970 kg (6,540 lb).
Height: 7.70 m (25.20 ft).
Diameter: 2.00 m (6.50 ft).
Thrust: 1,040.00 kN (233,800 lbf).
Burn time: 75 s.
Number: 2 .

More... - Chronology...


Associated Countries
Associated Engines
Associated Launch Vehicles
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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