Encyclopedia Astronautica
RH-300


ISRO solid rocket engine. 33.3 kN.

Gross mass: 300 kg (660 lb).
Unfuelled mass: 79 kg (174 lb).
Height: 2.80 m (9.10 ft).
Diameter: 0.31 m (1.01 ft).
Thrust: 33.30 kN (7,486 lbf).
Burn time: 16 s.

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Associated Countries
See also
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...

Associated Stages
  • RH-300-1 Solid rocket stage. 33.30 kN (7,486 lbf) thrust. Mass 300 kg (661 lb). More...

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