The Delta 4000 series was an American expendable launch system which was used to conduct two orbital launches in 1989 and 1990. It was a member of the Delta family of rockets.
Specifications
- Thrust
- 3,468 kN
- Height
- 34 m
- Diameter
- 2.44 m
- Launch mass
- 200 t
- Stages
- 4
- Launch cost
- $34.22M
- LEO capacity
- 3,400 kg
- GTO capacity
- 1,200 kg
- GEO capacity
- —
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
2
Launches with a definitive outcome
Success rate
100%
2 of 2
Current success streak
2
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 4925-8 | Insat 1D — Success
- Delta 4925-8 | Marcopolo 1 — Success