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Retired
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.
📊 Specifications
📏Height
21 m⭕Diameter
3.05 m⚖️Launch Mass
120 kg🛰️LEO Capacity
800 kg🌍GTO Capacity
—🗓️Maiden Flight
Sep 8, 1967🚀Total Launches
17✅Success Rate
88%♻️Reusable
Expendable🏭Manufacturer
Convair🌐Country
American📋Status
Retired📷 Photo Gallery