Encyclopedia Astronautica
RH-200-2


Solid rocket stage. 8.40 kN (1,888 lbf) thrust. Mass 20 kg (44 lb).

Status: Active.
Gross mass: 20 kg (44 lb).
Unfuelled mass: 11 kg (24 lb).
Height: 1.40 m (4.50 ft).
Diameter: 0.12 m (0.39 ft).
Thrust: 8.40 kN (1,888 lbf).
Burn time: 2.90 s.
Number: 808 .

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Associated Countries
Associated Engines
Associated Launch Vehicles
  • RH-200 Indian sounding rocket. Two stage vehicle consisting of 1 x RH-200 + 1 x RH-125 More...

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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