← Back to Rockets
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
Apr 6, 1973🚀Total Launches
32✅Success Rate
94%♻️Reusable
Expendable🏭Manufacturer
Convair🌐Country
American📋Status
Retired📷 Photo Gallery