Delta II 7920-10C
Delta family · United Launch Alliance · Retired
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
- 38.7 m
- Diameter
- 2.4 m
- Launch mass
- —
- Stages
- 2
- Launch cost
- $51M
- LEO capacity
- 5,959 kg
- GTO capacity
- 1,842 kg
- GEO capacity
- —
- SSO capacity
- 3,017 kg
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
17
Launches with a definitive outcome
Success rate
100%
17 of 17
Current success streak
17
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
- Delta II 7920-10C | NPP — Success
- Delta II 7920-10C | WorldView-2 — Success
- Delta II 7920-10C | STSS-DEMO/GMD — Success
- Delta II 7920-10C | STSS-ATRR/GMD (USA-205) — Success
- Delta II | Gravity Probe B — Success