Delta 5920-8 (McDonnell Douglas)
The Delta 5920-8 is a non-reusable, inactive launch vehicle manufactured by McDonnell Douglas. It undertook its inaugural launch on 11/18/1989.
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.
Delta 5920-8 Specifications
| Variant | 5920-8 |
|---|---|
| Length | 34 m |
| Diameter | 2.44 m |
| Stages | 3 |
| Launch Mass | 201 T |
| Takeoff Thrust | 3468 kN |
| LEO Capacity | 3848 kg |
| GTO Capacity | 1405 kg |
| Launch Cost | $34,220,000 |
Delta 5920-8 Launch Record
| Total Launches | 1 |
|---|---|
| Successful Launches | 1 |
| Consecutive Successful Launches | 1 |
Manufacturer
McDonnell Douglas (MDC)