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Delta II 7320

Delta familyUnited Launch AllianceRetired

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.

Delta II 7320 vehicle

Specifications

Thrust
2,552 kN
Height
38.9 m
Diameter
2.44 m
Launch mass
168 t
Stages
2
Launch cost
$51M
LEO capacity
2,800 kg
SSO capacity
1,650 kg

Specifications from Launch Library. Figures the operator has not published are omitted.

Flight record

6flightswith a definitive outcome
100%success rate6 of 6
6success streakcurrent

Counted from padside's own launch record, the same basis as the stats page.

Flights

5 of 6

All 6 flights