Encyclopedia Astronautica
RH-300/RH-200/RH-200


Indian sounding rocket. Three stage vehicle consisting of 1 x RH-300 + 1 x RH-200 + 1 x RH-200

Status: Retired 1985.
Gross mass: 500 kg (1,100 lb).
Height: 8.00 m (26.20 ft).
Diameter: 0.31 m (1.01 ft).
Thrust: 38.00 kN (8,542 lbf).
Apogee: 300 km (180 mi).
First Launch: 1985.11.01.
Number: 1 .

More... - Chronology...


Associated Countries
See also
  • RH Indian solid propellant sounding rocket family using indigenous rocket motors derived from French Belier / Jericho rocket engine technology. More...

Associated Manufacturers and Agencies
  • ISRO Indian manufacturer of rockets, spacecraft, and rocket engines. Indian Space Research Organization, India. More...

Associated Launch Sites
  • Sriharikota India's primary space launch center, located on the east coast of the peninsula with a firing sector over the Bay of Bengal. In use from 1971 to present. More...

Associated Stages
  • RH-200-1 Solid propellant rocket stage. Loaded mass 100 kg. Thrust 16.90 kN. More...
  • RH-300-1 Solid rocket stage. 33.30 kN (7,486 lbf) thrust. Mass 300 kg (661 lb). More...

RH-300/RH-200/RH-200 Chronology


1985 November 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-300/RH-200/RH-200.
  • Test mission - . Nation: India. Agency: ISRO. Apogee: 300 km (180 mi).

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