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SLV-3
Part of SLV
Indian all-solid orbital launch vehicle. Four stage vehicle consisting of 1 x SLV-3-1 + 1 x SLV-3-2 + 1 x SLV-3-3 + 1 x SLV-3-4

Status: Retired 1983. First Launch: 1979-08-10. Last Launch: 1983-04-17. Number: 4 . Payload: 42 kg (92 lb). Thrust: 503.00 kN (113,078 lbf). Gross mass: 17,000 kg (37,000 lb). Height: 23.60 m (77.40 ft). Diameter: 1.00 m (3.20 ft). Apogee: 900 km (550 mi).

LEO Payload: 42 kg (92 lb).



Family: all-solid, orbital launch vehicle. Country: India. Spacecraft: Rohini 1A, Rohini, Rohini 2. Launch Sites: Sriharikota, Sriharikota SLV. Stages: SLV-3 engine, SLV-1, SLV-2, SLV-4. Agency: Convair.

1979 August 10 - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLV. LV Family: SLV. Launch Vehicle: SLV-3. FAILURE: Thrust vectoring of second stage failed.. Failed Stage: 2.
1980 July 18 - . 02:33 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLV. LV Family: SLV. Launch Vehicle: SLV-3.
1981 May 31 - . 05:00 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLV. LV Family: SLV. Launch Vehicle: SLV-3. FAILURE: Partial Failure.. Failed Stage: U.
1983 April 17 - . 05:44 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLV. LV Family: SLV. Launch Vehicle: SLV-3.

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