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The Atlas-Agena was an American expendable launch system derived from the SM-65 Atlas missile. It was used to launch the first five Mariner uncrewed probes to the planets Venus and Mars, and the Ranger and Lunar Orbiter uncrewed probes to the Moon. The upper stage was also used as an uncrewed orbital target vehicle for the Gemini crewed spacecraft to practice rendezvous and docking. However, the launch vehicle family was originally developed for the Air Force and most of its launches were classified DoD payloads. The Atlas-Agena was a two-and-a-half-stage rocket, with a stage-and-a-half Atlas missile as the first stage, and an RM-81 Agena second stage. Initially, Atlas D missiles, redesignated as the LV-3, were used as the first stage. These were later replaced by the standardized Atlas SLV-3, and its derivatives, the SLV-3A and B. The final Atlas-Agena launch used an Atlas E/F.
Missions
109
Success Rate
83.9%
Successes
89
Failures
15
Success Streak
7
Partial Failures
5
Active in 1966
Stages
2
Active 1964 to 1967
Payload to Orbit
LEO: 1,825 kg
Stages
2
Active in 1966
Stages
2
Active 1968 to 1978
Stages
2
Active 1963 to 1965
Stages
2
Active 1961 to 1965
Payload to Orbit
LEO: 1,725 kg
Stages
2
Active 1960 to 1961
Payload to Orbit
LEO: 1,250 kg
Stages
2
Active in 1978
Stages
2