Delta II 7320-10C
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
- 38.9 m
- Diameter
- 2.44 m
- Launch mass
- 168 t
- Stages
- 2
- Launch cost
- $51M
- LEO capacity
- 2,800 kg
- GTO capacity
- —
- GEO capacity
- —
- SSO capacity
- 1,651 kg
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
6
Launches with a definitive outcome
Success rate
100%
6 of 6
Current success streak
6
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 7320-10C | SMAP, FIREBIRD II A, FIREBIRD II B, GRIFEX, ExoCube — Success
- Delta II 7320-10C | OCO-2 — Success
- Delta II 7320-10C | WISE — Success
- Delta II 7320-10C | NOAA-19 (NOAA N) — Success
- Delta II | NOAA 18 — Success