Delta 4925-8
Delta familyMcDonnell DouglasRetired
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
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
2flightswith a definitive outcome
100%success rate2 of 2
0failuresincluding partial failures
2success streakcurrent
First flight August 27, 1989 · latest June 12, 1990
Counted from padside's own launch record, the same basis as the stats page.
Flights per year
- Successful
- Failed
Show the numbers for Delta 4925-8 flights per year
| Year | Successful | Failed | Total |
|---|---|---|---|
| 1989 | 1 | 0 | 1 |
| 1990 | 1 | 0 | 1 |