Convair

SM-65B Atlas

B

Retired

Overview

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The Convair SM-65B Atlas, or Atlas B, also designated X-12 was a prototype of the Atlas missile. First flown on 19 July 1958, the Atlas B was the first version of the Atlas rocket to use the stage and a half design with an operational sustainer engine and jettisonable rocket booster section. Unlike later Atlas models, the Atlas B used explosive bolts to jettison the booster section.

Manufacturer

Convair

Variant

B

Alias

N/A

Maiden Flight

July 19, 1958

Technical Specifications

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31.4 m

Length

3.66 m

Diameter

0 t

Launch Mass

Liftoff Thrust

68 kg

LEO Capacity

GTO Capacity

Launch Record

/03
1

Total Launches

1

Successful

0

Failed

100.0%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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