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Atlas LV-3B

Atlas LV-3B

Atlas family · built by National Aeronautics and Space Administration · maiden flight 1960-07-29

Profile data last updated: 2026-08-29T15:37:07.354998+00:00 | 7531-10-18

The Atlas LV-3B, Atlas D Mercury Launch Vehicle or Mercury-Atlas Launch Vehicle, was a human-rated expendable launch system used as part of the United States Project Mercury to send astronauts into low Earth orbit. Manufactured by American aircraft manufacturing company Convair, it was derived from the SM-65D Atlas missile, and was a member of the Atlas family of rockets.

Specifications

28.7 mLength
3.0 mDiameter
120 tLaunch mass
1Stages
1300 kNLiftoff thrust

Payload Capacity

1360 kgTo LEO

Lifetime Launch Record

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

10Total launches
7Successful
3Failed
0Upcoming

Launches Tracked on This Site

10In our archive
70.0%Success rate
Sep 09, 1959 08:19 UTCEarliest tracked
May 15, 1963 13:04 UTCMost recent
MissionDateStatus
Atlas LV-3B | Mercury-Atlas 9 May 15, 1963 13:04 UTC Success
Atlas LV-3B | Mercury-Atlas 8 Oct 03, 1962 12:15 UTC Success
Atlas LV-3B | Mercury-Atlas 7 May 24, 1962 12:45 UTC Success
Atlas LV-3B | Mercury-Atlas 6 Feb 20, 1962 14:47 UTC Success
Atlas LV-3B | Mercury-Atlas 5 Nov 29, 1961 15:07 UTC Success
Atlas LV-3B | Mercury-Atlas 4 Sep 13, 1961 14:04 UTC Success
Atlas LV-3B | Mercury-Atlas 3 Apr 25, 1961 16:15 UTC Failure
Atlas LV-3B | Mercury-Atlas 2 Feb 21, 1961 14:10 UTC Success
Atlas LV-3B | Mercury-Atlas 1 Jul 29, 1960 13:13 UTC Failure
Atlas LV-3B | Big Joe 1 Sep 09, 1959 08:19 UTC Partial Failure

Wikipedia