National Aeronautics and Space Administration

Atlas LV-3B

LV-3B

Atlas LV-3B
Retired

Overview

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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.

Manufacturer

National Aeronautics and Space Administration

Variant

LV-3B

Alias

N/A

Maiden Flight

July 29, 1960

Technical Specifications

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28.7 m

Length

3 m

Diameter

0 t

Launch Mass

1300 kN

Liftoff Thrust

1360 kg

LEO Capacity

GTO Capacity

Launch Record

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10

Total Launches

7

Successful

3

Failed

70.0%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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