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Atlas SLV-3
Part of Atlas
Atlas SLV
Atlas SLV
Atlas SLV-3 s/n 7004 / Burner-2 (No Agena) - 1968-08-16
American orbital launch vehicle. Standardized Atlas booster with no or small solid upper stage.

AKA: SLV-3. Status: Retired 1967. First Launch: 1966-06-01. Last Launch: 1967-04-20. Number: 4 . Payload: 800 kg (1,760 lb). Thrust: 1,650.00 kN (370,930 lbf). Gross mass: 120,000 kg (260,000 lb). Height: 21.00 m (68.00 ft). Diameter: 3.05 m (10.00 ft). Apogee: 300 km (180 mi).

LEO Payload: 800 kg (1,760 lb) to a 300 km orbit at 28.00 degrees.


More at: SLV-3.

Family: orbital launch vehicle. Country: USA. Engines: LR105-5, LR89-5. Spacecraft: Gemini, Atlas Target Docking Adapter. Launch Sites: Cape Canaveral, Vandenberg, Cape Canaveral LC14, Vandenberg SLC3E. Stages: Atlas MA-3, Atlas Agena SLV-3. Agency: Convair.

1966 June 1 - . 15:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC14. LV Family: Atlas. Launch Vehicle: Atlas SLV-3.
1966 December 21 - . 22:15 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3E. LV Family: Atlas. Launch Vehicle: Atlas SLV-3.
1967 March 5 - . 23:05 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3E. LV Family: Atlas. Launch Vehicle: Atlas SLV-3.
1967 April 20 - . 01:35 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3E. LV Family: Atlas. Launch Vehicle: Atlas SLV-3.

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