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Atlas Centaur D
Part of Atlas
American orbital launch vehicle. Version with Centaur D upper stage.

Status: Retired 1967. First Launch: 1965-08-11. Last Launch: 1967-07-14. Number: 7 . Payload: 1,700 kg (3,700 lb). Gross mass: 136,100 kg (300,000 lb). Height: 33.00 m (108.00 ft). Diameter: 3.05 m (10.00 ft).

LEO Payload: 1,700 kg (3,700 lb). Payload: 1,700 kg (3,700 lb) to a GTO.



Family: orbital launch vehicle. Country: USA. Engines: LR105-5, LR89-7, RL-10A-3. Spacecraft: Surveyor. Launch Sites: Cape Canaveral, Cape Canaveral LC36A, Cape Canaveral LC36B. Stages: Centaur D/E, Atlas MA-2, Atlas D stage. Agency: Convair.

1965 August 11 - . 14:31 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36B. LV Family: Atlas. Launch Vehicle: Atlas Centaur D.
1966 April 8 - . 01:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36B. LV Family: Atlas. Launch Vehicle: Atlas Centaur D. FAILURE: Centaur propellant leak.. Failed Stage: U.
1966 May 30 - . 14:41 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36A. LV Family: Atlas. Launch Vehicle: Atlas Centaur D.
1966 September 20 - . 12:32 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36A. LV Family: Atlas. Launch Vehicle: Atlas Centaur D.
1966 October 26 - . 11:12 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36B. LV Family: Atlas. Launch Vehicle: Atlas Centaur D.
1967 April 17 - . 07:05 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36B. LV Family: Atlas. Launch Vehicle: Atlas Centaur D.
1967 July 14 - . 11:53 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36A. LV Family: Atlas. Launch Vehicle: Atlas Centaur D.

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