Padside

Delta II 7925H-9.5

Delta family · United Launch Alliance · Retired

Wikipedia ↗Compare with… →

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.

Specifications

Thrust
Height
38.9 m
Diameter
2.4 m
Launch mass
286 t
Stages
3
Launch cost
$51M
LEO capacity
GTO capacity
2,190 kg
GEO capacity
SSO capacity

Vehicle specifications from Launch Library; blanks are unpublished figures.

Flight record

Flights
3
Launches with a definitive outcome
Success rate
100%
3 of 3
Current success streak
3
Landings
0
0 attempts · 0 droneship / 0 RTLS
Fastest turnaround
Between consecutive booster flights

Counted from padside's own launch record — the same basis as the Stats page.

Launches