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Atlas V 421

Atlas V 421

Atlas family · built by United Launch Alliance · maiden flight 2007-10-11

Profile data last updated: 2026-08-15T20:08:04.839063+00:00 | 7531-09-02

Atlas V is an expendable launch system in the Atlas rocket family. It was formerly operated by Lockheed Martin and is now operated by United Launch Alliance (ULA), a joint venture with Boeing. Each Atlas V rocket uses a Russian-built RD-180 engine burning kerosene and liquid oxygen to power its first stage and an American-built RL10 engine burning liquid hydrogen and liquid oxygen to power its Centaur upper stage. The RD-180 engines are provided by RD Amross, while Aerojet Rocketdyne provides both the RL10 engines and the strap-on boosters used in some configurations. The 421 version uses a 4m wide fairing, 2 solid rocket boosters and one engine on the Centaur stage.

Specifications

58.3 mLength
3.8 mDiameter
433 tLaunch mass

Payload Capacity

14067 kgTo LEO
6890 kgTo GTO

Lifetime Launch Record

As reported by Launch Library 2 across this rocket's entire history, not just the launches tracked on this site.

9Total launches
9Successful
0Failed
0Upcoming

Launches Tracked on This Site

9In our archive
100.0%Success rate
Oct 11, 2007 00:22 UTCEarliest tracked
Aug 04, 2022 10:29 UTCMost recent
MissionDateStatus
Atlas V 421 | SBIRS GEO-6 Aug 04, 2022 10:29 UTC Success
Atlas V 421 | SBIRS GEO-5 May 18, 2021 17:37 UTC Success
Atlas V 421 | NROL-52 Oct 15, 2017 07:28 UTC Success
Atlas V 421 | NROL-61 Jul 28, 2016 12:37 UTC Success
Atlas V 421 | Mexsat-2 (Morelos III) Oct 02, 2015 10:28 UTC Success
Atlas V 421 | MMS Mar 13, 2015 02:44 UTC Success
Atlas V 421 | WGS-2 Apr 04, 2009 00:31 UTC Success
Atlas V 421 | ICO G1 Apr 14, 2008 20:12 UTC Success
Atlas V 421 | WGS-1 Oct 11, 2007 00:22 UTC Success

Official info · Wikipedia