Encyclopedia Astronautica
RH-200


ISRO solid rocket engine. 16.9 kN.

Gross mass: 100 kg (220 lb).
Height: 1.40 m (4.50 ft).
Diameter: 0.20 m (0.65 ft).
Thrust: 16.90 kN (3,799 lbf).
Burn time: 5.70 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-200-1 Solid propellant rocket stage. Loaded mass 100 kg. Thrust 16.90 kN. More...

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