|
Intermediate range ballistic missile. Year: 1995. IOC: 1995. Family: SLV. Country: India. 2 stage ballistic missile consisting of 1 x Agni + 1 x Prithvi Manufacturer: DRDE. Launches: 3. Failures: 1. Success Rate: 66.67%. First Launch Date: 1989-05-22. Last Launch Date: 1994-02-19. Launch data is: incomplete. Apogee: 300 km (180 mi). Liftoff Thrust: 503.000 kN (113,078 lbf). Total Mass: 13,600 kg (29,900 lb). Core Diameter: 1.31 m (4.29 ft). Total Length: 18.41 m (60.40 ft). Span: 1.31 m (4.29 ft). Standard warhead mass: 1,000 kg (2,200 lb). Maximum range: 1,200 km (700 mi). Boost Propulsion: Solid rocket. Cruise Propulsion: Storable liquid rocket.
Agni Chronology 1989 May 22 - 01:40 GMT - Launch Site: Balasore. Launch Vehicle: Agni. LV Configuration: Agni 01. - Test mission Nation: India. Agency: IDRDL. Apogee: 300 km (180 mi). References: 739.
1992 May 28 - Launch Site: Balasore. Launch Vehicle: Agni. LV Configuration: Agni 02. FAILURE: Failure. - Test mission Nation: India. Agency: IDRDL. Apogee: 10 km (6 mi). References: 739.
1994 February 19 - 12:13 GMT - Launch Site: Balasore. Launch Vehicle: Agni. LV Configuration: Agni 04. - Test mission Nation: India. Agency: IDRDL. Apogee: 300 km (180 mi). References: 739.
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.
|