Encyclopedia Astronautica
RH-300-1


Solid rocket stage. 33.30 kN (7,486 lbf) thrust. Mass 300 kg (661 lb).

Status: Retired 1993.
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.
Number: 19 .

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Associated Countries
Associated Engines
Associated Launch Vehicles
  • RH-560 Indian sounding rocket. 2 stage vehicle derived from French Stromboli engine technology. More...
  • RH-300 Indian sounding rocket. Sounding rocket derived from French Belier rocket engine technology. 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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