Delta II 7920-10 (United Launch Alliance)
The Delta II 7920-10 is a non-reusable, inactive launch vehicle manufactured by United Launch Alliance (established in 2006). It undertook its inaugural launch on 11/04/1995.
Delta II is an American space launch system developed by McDonnell Douglas, now part of the Delta rocket family operated by United Launch Alliance. With more than 150 missions and a nearly perfect track record, Delta II has established itself as one of the most successful orbital launch systems.
Delta II 7920-10 Specifications
| Variant | 7920-10 |
|---|---|
| Length | 38.7 m |
| Diameter | 2.4 m |
| Stages | 2 |
| Launch Mass | 251 T |
| LEO Capacity | 5959 kg |
| GTO Capacity | 1828 kg |
| SSO Capacity | 3017 kg |
| Launch Cost | $51,000,000 |
Delta II 7920-10 Launch Record
| Total Launches | 9 |
|---|---|
| Successful Launches | 9 |
| Consecutive Successful Launches | 9 |
Manufacturer
CEO: Mark Peller
United Launch Alliance (ULA) is a joint venture of Lockheed Martin Space Systems and Boeing Defense, Space & Security. ULA was formed in December 2006 by combining the teams at these companies which provide spacecraft launch services to the government of the United States. ULA launches from both coasts of the US. They launch their Atlas V vehicle from LC-41 in Cape Canaveral and LC-3E at Vandeberg. Their Delta IV launches from LC-37 at Cape Canaveral and LC-6 at Vandenberg.