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HomeLaunch HistoryRocket EncyclopediaFuture LaunchesStatistics & ChartsDashboard

Atlas family

Atlas SLV-3C Centaur

United States1967 to 1972
Drawing of the Atlas SLV-3C Centaur

The improved Atlas-Centaur of the late 1960s. It launches the last Surveyors, the Mariner 6, 7 and 9 Mars missions, Mariner 9 becoming the first spacecraft to orbit another planet, Pioneer 10, the first probe to Jupiter, and Intelsat IV satellites.

Launches
17
Success rate
82%
2 failures · 1 partial
First flight
8 September 1967
Surveyor 5
Last flight
21 August 1972
Copernicus
Builder
Convair
Height
40.2 m
Diameter
3.1 m
Stages
2
Boosters
1 × Atlas Booster
Propellants
Kerosene / LOX, LH2 / LOX
Payload to LEO
800 kg
Payload to GTO
1,800 kg

Launches per year

Atlas SLV-3C Centaur
Other Atlas rockets
Show as table
YearLaunchesAtlas SLV-3C Centaur
195810
195910
196050
1961110
1962160
1963100
1964180
1965190
1966330
1967142
196883
196953
197031
197164
197264
197340
197420
197550
197640
197770
1978140
197940
198080
198160
198230
198360
198450
198550
198630
198730
198820
198910
199030
199140
199250
199360
199470
1995120
199670
199780
199860
199950
200080
200140
200250
200350
200460
200530
200620
200740
200820
200950
201040
201150
201260
201380
201490
201590
201680
201760
201850
201920
202050
202140
202270
202320
202420
202550
202640

Atlas rockets

RocketFlownLaunchesSuccess rateHeightPayload to LEO
SM-65B Atlas19581100%22 m68 kg
Atlas-Able1959 to 196030%35 m625 kg
Atlas LV-3 Agena A1960333%30 m1,000 kg
Atlas LV-3 Agena B1961 to 19652976%32.1 m1,725 kg
Atlas LV-3B1961 to 1963786%28.7 m1,360 kg
Atlas LV-3 Agena D1963 to 196515100%32.1 m1,000 kg
Atlas LV-3C Centaur1963 to 1965450%33 m
Atlas SLV-3 Agena D1964 to 19674892%32.1 m1,000 kg
SM-65D Atlas1965 to 1967743%25.2 m1,400 kg
Atlas LV-3C Centaur D1965 to 19677100%33 m
Atlas SLV-319661100%21 m800 kg
Atlas SLV-3 Agena B19661100%32.1 m1,000 kg
Atlas SLV-3C Centaur1967 to 19721782%40.2 m800 kg
Atlas SLV-3A Agena D1968 to 19781292%36 m1,000 kg
SM-65F Atlas1968 to 1981989%20 m820 kg
Atlas SLV-3 Burner-21968 to 1972250%28.9 m800 kg
Atlas SLV-3D Centaur1973 to 19833291%40.3 m800 kg
Atlas F/PTS19741100%29.2 m295 kg
Atlas F MSD1976 to 19803100%27.3 m800 kg
Atlas F/SVS1977 to 19807100%29.2 m820 kg
Atlas F/Agena D19781100%34.6 m1,000 kg
Atlas F/OIS19791100%32.1 m870 kg
Atlas E MSD198010%27.3 m800 kg
Atlas E/SVS198110%29.2 m800 kg
SM-65E Atlas1982 to 199515100%20 m820 kg
Atlas H1983 to 19875100%27 m3,630 kg
Atlas E/SGS-21983 to 19854100%32.1 m455 kg
Atlas G Centaur1984 to 1989771%41.8 m3,630 kg
Atlas E/OIS19851100%28.7 m870 kg
Atlas E Altair19901100%27.3 m210 kg
Atlas I1990 to 19971173%43.9 m5,900 kg
Atlas II1991 to 199810100%47.5 m6,580 kg
Atlas IIA1992 to 200223100%47.5 m6,580 kg
Atlas IIAS1993 to 200430100%47.5 m6,580 kg
Atlas IIIA2000 to 20042100%52.8 m8,640 kg
Atlas IIIB2002 to 20054100%52.8 m10,218 kg
Atlas V 4012002 to 20224198%58.3 m9,050 kg
Atlas V 5212003 to 20042100%58.3 m13,490 kg
Atlas V 4312005 to 20163100%59.1 m15,260 kg
Atlas V 5512006 to 202623100%59.7 m18,850 kg
Atlas V 4112006 to 20206100%58.3 m8,080 kg
Atlas V 4212007 to 20229100%58.3 m14,067 kg
Atlas V 5012010 to 20238100%58.3 m8,210 kg
Atlas V 5312010 to 20225100%60 m15,530 kg
Atlas V 5412011 to 20229100%60 m17,410 kg
Atlas V N222019 to 20243100%52.4 m13,034 kg
Atlas V 51120221100%58.3 m10,986 kg