Indian sounding rocket. Three stage vehicle consisting of 1 x RH-300 + 1 x RH-200 + 1 x RH-200
Status: Retired 1985.
More... - Chronology...
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 .
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...
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...
1985 November 1 -
. LV Family
. Launch Vehicle
- Test mission - .
Nation: India. Agency: ISRO. Apogee: 300 km (180 mi).
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