RH-300 Mk II
Sounding rocket. Year: 1987. Family: Belier. Country: India.

Single stage vehicle

Manufacturer: ISRO. Launches: 4. Failures: 1. Success Rate: 75.00%. First Launch Date: 1987-06-08. Last Launch Date: 1999-11-20. Launch data is: continuing. Apogee: 150 km (90 mi). Liftoff Thrust: 39.000 kN (8,767 lbf). Total Mass: 500 kg (1,100 lb). Core Diameter: 0.31 m (1.01 ft). Total Length: 5.90 m (19.30 ft).



RH-300 Mk II Chronology

1987 June 8 - Launch Site: Sriharikota. Launch Vehicle: RH-300 Mk II.

  • Test mission Nation: India. Agency: ISRO. Apogee: 130 km (80 mi). References: 1173.
1997 November 20 - 17:30 GMT - Launch Site: SvalRak. Launch Vehicle: RH-300 Mk II. LV Configuration: RH-300 Mk II F-110. FAILURE: Failure.
  • ISBJORN-1 Ionosphere mission Nation: Norway. Agency: NDRE. Apogee: 71 km (44 mi). References: 1887.
1999 November 18 - 01:55 GMT - Launch Site: Sriharikota. Launch Vehicle: RH-300 Mk II.
  • LMS Ionosphere/Meteor mission Nation: India. Agency: ISRO. Apogee: 135 km (83 mi). References: 1677.
1999 November 20 - 01:35 GMT - Launch Site: Sriharikota. Launch Vehicle: RH-300 Mk II.
  • LMS Ionosphere/Meteor mission Nation: India. Agency: ISRO. Apogee: 135 km (83 mi). References: 1677.

Bibliography and Further Reading
  • McDowell, Jonathan, Jonathan's Space Home Page, Harvard University, 1997-present. Jonathan McDowell's complete on-line listing of all objects orbited and over 20,000 rocket launches Accessed at: http://www.planet4589.org/jsr.html.
 
 
 
 
 
 
 
 
 

Contact us with any corrections, additions, or comments.
Conditions for use of drawings, pictures, or other materials from this site..
To contact astronauts or cosmonauts.

© Mark Wade, 1997 - 2007 except where otherwise noted.

 
Encyclopedia Astronautica
topic index
0 - A - B - C - D - E - F - G - H - I - J - K - L - M - N - O - P - Q - Ra - Re - Sa - Sf - Sp - T - U - V - W - X - Y - Z