Atlas G
| Status | Retired |
|---|---|
| Rocket family | Atlas |
| Country | United States |
| Manufacturer | Lockheed |
| Number of orbital launches | 7 |
| First launch | 1984-06-09 |
| Last launch | 1989-09-25 |
Launches by year:
Launches:
| Launch date | Launch site | Rocket / Variant | Payload | Notes | Status |
|---|---|---|---|---|---|
| 1989-09-25 | Cape Canaveral | Atlas G Centaur-D1AR | FLTSATCOM 8 (USA 46) | success | |
| 1987-03-26 | Cape Canaveral | Atlas G Centaur-D1AR | FLTSATCOM 6 | failure | |
Lightning strike zapped guidance at T+51 seconds. Fault was directly attributed to a random memory upset that forced rocket to veer off course. Destroyed by range safety. | |||||
| 1986-12-05 | Cape Canaveral | Atlas G Centaur-D1AR | FLTSATCOM 7 (USA 20) | success | |
| 1985-09-28 | Cape Canaveral | Atlas G Centaur-D1AR | Intelsat-5A 12 | success | |
| 1985-06-30 | Cape Canaveral | Atlas G Centaur-D1AR | Intelsat-5A 11 | success | |
| 1985-03-22 | Cape Canaveral | Atlas G Centaur-D1AR | Intelsat-5A 10 | success | |
| 1984-06-09 | Cape Canaveral | Atlas G Centaur-D1AR | Intelsat-5 9 | pfailure | |
Centaur structural failure. | |||||
Variants:
(This section is under construction)Atlas G Centaur-D1AR
| First launch | 1984-06-09 |
|---|---|
| Mass | 166.14 t |
| Height | 38 m |
Payload capacity:
| LEO | 3630 kg to 185 km |
|---|---|
| GTO | 2255 kg |
