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The three-stage core vehicle was essentially the same as the Delta C. 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. An Altair-2 SRM was used as a third stage. The main difference between the Delta C and Delta D was the presence of three Castor-1 solid rocket boosters, clustered around the first stage.
Missions
2
Success Rate
100.0%
Successes
2
Failures
0
Success Streak
2
Partial Failures
0
Active 1964 to 1965
Payload to Orbit
LEO: 575 kg
GTO: 104 kg
Liftoff Thrust
1,725 Kilonewtons
Stages
3
Strap-ons
3