The Delta 5000 series was an American expendable launch system which was used to conduct an orbital launch in 1989. It was a member of the Delta family of rockets. Although several variants were put forward, only the Delta 5920 was launched.
Specifications
- Thrust
- 3,468 kN
- Height
- 34 m
- Diameter
- 2.44 m
- Launch mass
- 201 t
- Stages
- 3
- Launch cost
- $34.22M
- LEO capacity
- 3,848 kg
- GTO capacity
- 1,405 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Vehicle specifications from Launch Library; blanks are unpublished figures.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
- Delta 5920-8 | COBE — Success