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Atlas · Convair

Atlas LV-3B

retired
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Specifications

Status
retired
Height
28.7 m
Diameter
3 m
Mass
120,000 kg
Stages
1
Payload to LEO
1,360 kg
First flight
1960-07-29
Total launches
10
Success / Fail
7 / 3

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.

Payloads it launched · 6

MERCURY ATLAS 9
LEO
MERCURY ATLAS 8
LEO
MERCURY ATLAS 7
LEO
MERCURY ATLAS 6
LEO
MERCURY ATLAS 5
Payload
MERCURY ATLAS 4
LEO