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Delta II 7920-10

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 7920-10 vehicle

Specifications

Thrust
4,049 kN
Height
38.7 m
Diameter
2.4 m
Launch mass
251 t
Stages
2
Launch cost
$51M
LEO capacity
5,959 kg
GTO capacity
1,828 kg
SSO capacity
3,017 kg

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

Flight record

9flightswith a definitive outcome
100%success rate9 of 9
9success streakcurrent

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

Flights

5 of 9

All 9 flights