Delta II
In-activeUnited Launch Alliance (ULA)
Feb. 17, 2007
Description
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.
Specifications
-
Stages
3 -
Length
38.9 m -
Diameter
2.4 m -
Fairing Diameter
3.0 m -
Launch Mass
286.0 T -
Thrust
―
Family
-
Name
Delta II -
Family
― -
Variant
7925-10C -
Alias
― -
Full Name
Delta II 7925-10C
Payload Capacity
-
Launch Cost
$51000000 -
Low Earth Orbit
― -
Geostationary Transfer
Orbit
1840.0 kg -
Direct Geostationary
― -
Sun-Synchronous Capacity
―
United Launch Alliance
Commercial
Interim CEO: John Elbon
ULA 2006United 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.
Delta II 7925-10C | THEMIS
United Launch Alliance | United States of AmericaCape Canaveral SFS, FL, USA
Feb. 17, 2007, 11:01 p.m.
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