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Delta · McDonnell Douglas

Delta II 7925-10C

retired
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Specifications

Status
retired
Height
38.9 m
Diameter
2.4 m
Mass
286,000 kg
Stages
3
Payload to GTO
1,840 kg
First flight
2007-02-17
Total launches
1
Success / Fail
1 / 0

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.

Payloads it launched · 5

THEMIS D
HEO
THEMIS E
HEO
ARTEMIS P1 (THEMIS B)
Lunar
ARTEMIS P2 (THEMIS C)
Lunar
THEMIS A
HEO