Delta C
| Status | Retired |
|---|---|
| Rocket family | Delta |
| Country | United States |
| Manufacturer | Douglas |
| Number of orbital launches | 10 |
| First launch | 1963-11-27 |
| Last launch | 1967-03-08 |
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Launches by year:
Launches:
| Launch date | Launch site | Rocket / Variant | Payload | Notes | Status |
|---|---|---|---|---|---|
| 1967-03-08 | Cape Canaveral | Delta C | OSO 3 | success | |
| 1966-02-03 | Cape Canaveral | Delta C | ESSA 1 | success | |
| 1965-08-25 | Cape Canaveral | Delta C | OSO C | failure | |
Premature third stage ignition. | |||||
| 1965-07-02 | Cape Canaveral | Delta C | TIROS 10 | success | |
| 1965-05-29 | Cape Canaveral | Delta C | Explorer 28 (IMP 3) | success | |
| 1965-02-03 | Cape Canaveral | Delta C | OSO 2 | success | |
| 1965-01-22 | Cape Canaveral | Delta C | TIROS 9 | failure | |
| 1964-12-21 | Cape Canaveral | Delta C | Explorer 26 (EPE-D) | success | |
| 1964-10-04 | Cape Canaveral | Delta C | Explorer 21 (IMP 2) | success | |
| 1963-11-27 | Cape Canaveral | Delta C | Explorer 18 (IMP 1) | success | |
Variants:
(This section is under construction)Delta C Base variant (Delta DSV-3C)
| First launch | 1963-11-27 |
|---|---|
| Stages | 3 |
| Boosters | 0 |
| Mass | 52 t |
| Height | 27.5 m |
Payload capacity:
| LEO | 410 kg |
|---|
The first member of the Delta series to incorporate the X258 motor.