Delta 3910/PAM (McDonnell Douglas)
The Delta 3910/PAM is a non-reusable, inactive launch vehicle manufactured by McDonnell Douglas. It undertook its inaugural launch on 11/15/1980.
The Delta 3000 series was an American expendable launch system which was used to conduct 38 orbital launches between 1975 and 1989. It was a member of the Delta family of rockets. Several variants existed, which were differentiated by a four digit numerical code.
Delta 3910/PAM Specifications
| Variant | 3910/PAM |
|---|---|
| Length | 35 m |
| Diameter | 2.44 m |
| Stages | 4 |
| Launch Mass | 191 T |
| Takeoff Thrust | 3188 kN |
| LEO Capacity | 1087 kg |
Delta 3910/PAM Launch Record
| Total Launches | 7 |
|---|---|
| Successful Launches | 7 |
| Consecutive Successful Launches | 7 |
Manufacturer
McDonnell Douglas (MDC)