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UNITED LAUNCH ALLIANCE

Delta II

9FLIGHTS

100%SUCCESS

2STREAK

Mar 2008FIRST FLIGHT

NOREUSABLE

HEIGHT38.9 m

DIAMETER2.4 m

LAUNCH MASS256 kg

STAGES2

ABOUT DELTA II

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.

PAYLOAD CAPACITY

5,959 kg

TO LEO

13,140 lbs

2,120 kg

TO GTO

4,675 lbs

DIMENSIONS

↕Height38.9 m (128 ft)

↔Diameter2.4 m (7.9 ft)

⚖Launch Mass256 kg (564 lbs)

▣Stages2

🔗 WIKIPEDIA 🔗 OFFICIAL INFO

FLIGHT HISTORY

Delta II 7920-10 | JPSS 1 (Joint Polar Satellite System spacecraft No. 1)

Nov 18, 2017SUCCESS

Delta II 7320-10C | SMAP, FIREBIRD II A, FIREBIRD II B, GRIFEX, ExoCube

Jan 31, 2015SUCCESS

Delta II 7320-10C | OCO-2

Jul 2, 2014SUCCESS

Delta II 7920-10C | NPP

Oct 28, 2011SUCCESS

Delta II 7920H-10C | GRAIL-A (Ebb) & GRAIL-B (Flow)

Sep 10, 2011SUCCESS

Delta II 7320 | SAC-D

Jun 10, 2011SUCCESS

Delta II 7420-10 | COSMO-SkyMed 1

Jun 8, 2007SUCCESS

Delta II 7925-10C | THEMIS

Feb 17, 2007SUCCESS

Delta II 7920-10 | NROL-21

Dec 14, 2006SUCCESS

Delta II | GPS IIR-16(M)

Nov 17, 2006SUCCESS

Delta II | STEREO A & B

Oct 26, 2006SUCCESS

Delta II | GPS IIR-15(M)

Sep 25, 2006SUCCESS

Delta II | MITEx

Jun 21, 2006SUCCESS

Delta 7420-10C | Cloudsat

Apr 28, 2006SUCCESS

Delta II | GPS IIR-14(M)

Sep 26, 2005SUCCESS

⚙ RELATED ENGINES

RS-68AEngine RL-10Engine

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