Encyclopedia Astronautica
RH-300-II


ISRO solid rocket engine. 39.1 kN.

Gross mass: 500 kg (1,100 lb).
Height: 3.40 m (11.10 ft).
Diameter: 0.31 m (1.01 ft).
Thrust: 39.10 kN (8,790 lbf).
Burn time: 20 s.

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Associated Countries
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Associated Manufacturers and Agencies
  • ISRO Indian manufacturer of rockets, spacecraft, and rocket engines. Indian Space Research Organization, 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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