Atlas IIA
| Status | retired |
|---|---|
| Rocket family | Atlas |
| Country | United States |
| Manufacturer | Lockheed |
| Number of launches | 23 |
| First launch | 1992-06-10 |
| Last launch | 2002-12-05 |
Launches by year:
Latest launches:
| Launch date | Launch site | Rocket / Variant | Payload | Status |
|---|---|---|---|---|
| 2002-12-05 | Cape Canaveral | Atlas IIA | TDRS 10 (J) | success |
| 2002-03-08 | Cape Canaveral | Atlas IIA | TDRS 9 (I) | success |
| 2001-07-23 | Cape Canaveral | Atlas IIA | GOES 12 (M) | success |
| 2000-10-20 | Cape Canaveral | Atlas IIA | DSCS-3 B11 (USA 153) [IABS] | success |
| 2000-06-30 | Cape Canaveral | Atlas IIA | TDRS 8 (H) | success |
| 2000-05-03 | Cape Canaveral | Atlas IIA | GOES 11 (L) | success |
| 2000-01-21 | Cape Canaveral | Atlas IIA | DSCS-3 B8 (USA 148) [IABS] | success |
| 1999-11-23 | Cape Canaveral | Atlas IIA | UFO 10 (USA 146) | success |
| 1998-10-20 | Cape Canaveral | Atlas IIA | UFO 9 (USA 141) | success |
| 1998-10-09 | Cape Canaveral | Atlas IIA | Hotbird 5 | success |
Variants:
(This section is under construction)Atlas IIA
| First launch | 1992-06-10 |
|---|---|
| Upper stage | Centaur IIA |
| Mass | 185.43 t |
| Height | 47.4 m |
Payload capacity:
| LEO | 7300 kg to 185 km / 28.5 deg |
|---|---|
| GTO | 3140 kg |