Encyclopedia Astronautica
RH-300 Mk II-1


Solid propellant rocket stage. Loaded mass 500 kg. Thrust 39.10 kN.

Status: Active.
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.
Number: 13 .

More... - Chronology...


Associated Countries
Associated Engines
Associated Launch Vehicles
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...

Home - Browse - Contact
© / Conditions for Use