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Space · launch vehicle

Delta II 7920H

ULA RETIRED
At a glance
Launches
1
Success rate
100%
1 ok · 0 failed
Payload to LEO
5,959 kg
Payload to GTO
2,120 kg
Status
Retired
First flight
25 Aug 2003
Reusable
No
Height
38.9 m
Diameter
2.44 m
Launch mass
232 t
Liftoff thrust
—
Stages
2
Launch cost
$51,000,000
Booster landings
—
About

Delta II is an American space launch system developed by McDonnell Douglas, now part of the Delta rocket family operated by United Launch Alliance. With more than 150 missions and a nearly perfect track record, Delta II has established itself as one of the most successful orbital launch systems.