Rocket Details

In-depth specifications and launch history

Delta II 7925-10C

Delta II 7925-10C

Delta Family

About This Rocket

No detailed information available for this rocket.

Physical Specifications

Height38.9 m
Diameter2.4 m
Launch Mass286 kg
Stages3

Performance

LEO CapacityN/A kg
GTO Capacity1,840 kg
ThrustN/A kN
Launch Cost$51,000,000

Manufacturer

United Launch Alliance logo

United Launch Alliance

(ULA)

CommercialUSAFounded 2006

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.

Total Launches

160

Success: 160Failed: 0

Success Rate

100.0%

Landing Success

0%

0/0 attempts

AdministratorCEO: Tory Bruno
Vehicle FamilyAtlas | Delta IV | Vulcan
SpacecraftCST-100 Starliner
Consecutive Successes160

Technical Information

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.

ReusableNo

Launch Statistics

Maiden FlightFeb 17, 2007
Total Launches1
Success: 1Failed: 0
Landing Success0/0

Additional Information

Variant7925-10C
Consecutive Successes1