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The Delta 4000-series and 5000-series were developed in the aftermath of the Challenger disaster and consisted of a combination of 3000-era and Delta II-era components. The first stage had the MB-3 main engine and Extended Long Tank of the 3000-series and mounted upgraded Castor 4A motors. The new Delta K second stage was also included.
Missions
2
Success Rate
100.0%
Successes
2
Failures
0
Success Streak
2
Partial Failures
0
Active 1989 to 1990
Rocket
Height: 34m
Payload to Orbit
LEO: 3,400 kg
GTO: 1,200 kg
Liftoff Thrust
3,469 Kilonewtons
Fairing
Diameter: 2.44m
Stages
3
Strap-ons
9