DRDO solid rocket engine. 700 kN.
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.
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Associated Countries
See also
Associated Manufacturers and Agencies
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DRDO Indian manufacturer of rocket engines. DRDO, India. More...
Associated Propellants
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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
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Agni 2-1 Solid rocket stage. 700.00 kN (157,366 lbf) thrust. Mass 11,500 kg (25,353 lb). More...
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