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The first stage was a Thor missile in the DSV-2A configuration, and the second stage was the Delta D, which was derived from the earlier Delta. The baseline Delta C used an Altair-2 third stage, whilst the Delta C1 had an FW-4D third stage, which provided a higher payload capacity than the Altair. It is unclear whether two or three launches were made using the C1 configuration.
Missions
13
Success Rate
88.5%
Successes
11
Failures
1
Success Streak
5
Partial Failures
1
Active 1966 to 1969
Payload to Orbit
LEO: 600 kg
Stages
3
Active 1963 to 1967
Rocket
Height: 31m
Payload to Orbit
LEO: 410 kg
GTO: 82 kg
Liftoff Thrust
667 Kilonewtons
Stages
3