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Atlas·Convair

Atlas LV-3C Centaur

retired
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Specifications

Status
retired
Height
33 m
Diameter
3.05 m
Stages
2
Thrust
1,704 kN
Payload to GTO
1,800 kg
First flight
1962-05-08
Total launches
4
Success / Fail
2 / 2

The Atlas-Centaur was a US expendable launch vehicle derived from the SM-65 Atlas D missile. Launches were conducted from Launch Complex 36 at the Cape Canaveral Air Force Station in Florida.

Payloads it launched

1 loaded
ATLAS CENTAUR 2
LEO