Atlas·Convair
Atlas SLV-3D 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
- 1973-04-06
- Total launches
- 32
- Success / Fail
- 30 / 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
35 loaded
INTELSAT 506
GEO
INTELSAT 505
GEO
INTELSAT 504
GEO
INTELSAT 503
GEO
FLTSATCOM 5
GEO
INTELSAT 501
GEO
ESIAFI 1 (COMSTAR 4)
GEO
INTELSAT 502
GEO
OPS 6394 (FLTSATCOM 4)
GEO
OPS 6393 (FLTSATCOM 3)
GEO
HEAO 3
LEO
OPS 6392 (FLTSATCOM 2)
GEO
HEAO 2
LEO
PIONEER VENUS PROBE BUS
Venus
PIONEER VENUS PROBE 2
Venus
PIONEER VENUS PROBE 1
Venus
PIONEER VENUS PROBE 3
Venus
PIONEER VENUS PROBE 4
Venus
COMSTAR 3
GEO
PIONEER VENUS ORBITER
Venus
INTELSAT 4A-F6
GEO
OPS 6391 (FLTSATCOM 1)
GEO
INTELSAT 4A-F3
GEO
COSMOS 957
LEO
HEAO 1
LEO
INTELSAT 4A-F4
GEO
COMSTAR 2
GEO
COMSTAR 1
GEO
INTELSAT 4A-F2
GEO
INTELSAT 4A-F1
GEO
INTELSAT 4-F1
GEO
INTELSAT 4-F8
GEO
MARINER 10 (MVM-73)
Heliocentric
INTELSAT 4-F7
GEO
PIONEER 11
Interstellar