Atlas II
| Use attributes for filter ! | |
| Mass | 204,300 kg |
|---|---|
| Payload to leo | 6,580 kg |
| First flight | II: December 7, 1991; IIA: June 10, 1992; IIAS: December 16, 1993 |
| Stages | 3. 5 |
| Manufacturers | Lockheed Martin |
| Launch sites | Spaceport Florida Launch Complex 36 |
| Date of Reg. | |
| Date of Upd. | |
| ID | 2951963 |
About Atlas II
Atlas II was a member of the Atlas family of launch vehicles, which evolved from the successful Atlas missile program of the 1950s. It was designed to launch payloads into low earth orbit, geosynchronous transfer orbit or geosynchronous orbit.
