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Agni TD
Part of ASLV
Indian intermediate range ballistic missile. Two stage test missile consisting of 1 x Agni (developed from first stage of the SLV-3 space launcher) + 1 x Prithvi upper stage. Development began in 1979 and fewer than 10 systems were produced. Flight tests in 1989-1994 before the program was terminated.
Status: Retired 1994. First Launch: 1989-05-22. Last Launch: 1994-02-19. Number: 3 . Gross mass: 19,000 kg (41,000 lb). Height: 21.00 m (68.00 ft). Diameter: 1.00 m (3.20 ft). Apogee: 300 km (180 mi).
Maximum range: 1,200 km (700 mi).
Family:
IRBM.
Country:
India.
Launch Vehicles:
Agni.
Launch Sites:
Balasore.
Stages:
Agni engine,
Prithvi engine.
Agency:
DRDE.
1989 May 22 - .
01:40 GMT - .
Launch Site:
Balasore.
LV Family:
ASLV.
Launch Vehicle:
Agni TD.
- Test mission - .
Nation: India.
Agency: IDRDL.
Apogee: 300 km (180 mi).
1992 May 28 - .
Launch Site:
Balasore.
LV Family:
ASLV.
Launch Vehicle:
Agni TD.
FAILURE: Failure.
- Test mission - .
Nation: India.
Agency: IDRDL.
Apogee: 10 km (6 mi).
1994 February 19 - .
12:13 GMT - .
Launch Site:
Balasore.
LV Family:
ASLV.
Launch Vehicle:
Agni TD.
- Agni RV Mk 1 - .
Nation: India.
Agency: IDRDL.
Apogee: 300 km (180 mi).
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