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SLV
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SLV-3
SLV-3
Indian all-solid orbital launch vehicle.

AKA: Satellite Launch Vehicle. Status: Retired 1983. Payload: 40 kg (88 lb). Thrust: 454.90 kN (102,266 lbf). Gross mass: 17,610 kg (38,820 lb). Height: 24.00 m (78.00 ft). Diameter: 1.00 m (3.20 ft). Apogee: 400 km (240 mi).

LEO Payload: 40 kg (88 lb) to a 400 km orbit. Flyaway Unit Cost 1985$: 5.000 million.

Stage Data - SLV


More at: SLV.

Subtopics

SLV-3 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

SLV-3 D4 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 AS-4

Family: all-solid, orbital launch vehicle. Country: India. Spacecraft: Rohini 1A, Rohini, Rohini 2. Stages: SLV-3 engine, SLV-1, SLV-2, SLV-4. Agency: ISRO. Bibliography: 2, 42, 5, 6, 61.

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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