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The first stage was a Thor missile in the DM-21 configuration, and the second stage was the Delta A, an uprated version of the original Delta. An Altair solid rocket motor was used as a third stage.
Missions
2
Success Rate
100.0%
Successes
2
Failures
0
Success Streak
2
Partial Failures
0
Active in 1962
Payload to Orbit
LEO: 320 kg
GTO: 68 kg
Stages
3