Delta D
| Status | Retired |
|---|---|
| Rocket family | Delta |
| Country | United States |
| Manufacturer | Douglas |
| Number of orbital launches | 2 |
| First launch | 1964-08-19 |
| Last launch | 1965-04-06 |
Launches:
| Launch date | Launch site | Rocket / Variant | Payload | Notes | Status |
|---|---|---|---|---|---|
| 1965-04-06 | Cape Canaveral | Delta D | Intelsat-1 1 (Early Bird) | success | |
| 1964-08-19 | Cape Canaveral | Delta D | Syncom 3 | success | |
Variants:
(This section is under construction)Delta D (Delta DSV-3D)
| First launch | 1964-08-19 |
|---|---|
| Stages | 3 |
| Boosters | 3 x Thiokol Castor TX-345-5 |
| Mass | 63.97 t |
| Height | 32 m |
Payload capacity:
| LEO | 576 kg |
|---|---|
| GTO | 104 kg |
Introduced the Thrust-Augmented Thor that was being used for Thor-Agena missions, with an MB-3-3 engine and three Castor-1 boosters.