火箭详情
基本信息
| 名称 |
Atlas IIAS |
| 全名 |
Atlas IIAS |
| 家族 |
Atlas, Atlas II |
| 型号 |
IIAS |
| 制造商 |
Lockheed Martin |
规格参数
| 长度 |
47.54 m |
| 直径 |
3.04 m |
| 最小级数 |
3 |
| 最大级数 |
3 |
| 起飞质量 |
204 t |
| 起飞推力 |
4391 kN |
| LEO运力 |
6580 kg |
| GTO运力 |
2810 kg |
| 首飞时间 |
1993-12-16 |
描述
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. Sixty-three launches of the Atlas II, IIA and IIAS models were carried out between 1991 and 2004; all sixty-three launches were successes, making the Atlas II the most reliable launch system in history.
