Padside

Delta II 7920H

Delta family · United Launch Alliance · Retired

Wikipedia ↗Official ↗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
2.44 m
Launch mass
232 t
Stages
2
Launch cost
$51M
LEO capacity
5,959 kg
GTO capacity
2,120 kg
GEO capacity
SSO capacity

Vehicle specifications from Launch Library; blanks are unpublished figures.

Flight record

Flights
1
Launches with a definitive outcome
Success rate
100%
1 of 1
Current success streak
1
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