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Atlas · Convair

Atlas SLV-3C Centaur

retired
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Specifications

Status
retired
Height
21 m
Diameter
3.05 m
Mass
120,000 kg
Stages
2
Payload to LEO
800 kg
First flight
1967-09-08
Total launches
17
Success / Fail
15 / 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 · 15

OAO 3 (COPERNICUS)
LEO
INTELSAT 4-F5
GEO
PIONEER 10
Interstellar
INTELSAT 4-F4
GEO
INTELSAT 4-F3
GEO
MARINER 9
Mars
INTELSAT 4-F2
GEO
ATS 5
GEO
MARINER 7
Heliocentric
MARINER 6
Heliocentric
OAO 2
LEO
ATS 4
LEO
SURVEYOR 7
Lunar
SURVEYOR 6
Lunar
SURVEYOR 5
Lunar