National Aeronautics and Space Administration

Saturn IB

IB

Saturn IB
Retired

Overview

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The Saturn IB (pronounced "one B", also known as the Uprated Saturn I) was an American launch vehicle commissioned by the National Aeronautics and Space Administration (NASA) for the Apollo program. It replaced the S-IV second stage of the Saturn I with the much more powerful S-IVB, able to launch a partially fueled Apollo Command/Service Module (CSM) or a fully fueled Lunar Module (LM) into low Earth orbit for early flight tests before the larger Saturn V needed for lunar flight was ready.

Manufacturer

National Aeronautics and Space Administration

Variant

IB

Alias

N/A

Maiden Flight

February 26, 1966

Technical Specifications

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43.2 m

Length

6.61 m

Diameter

1 t

Launch Mass

7100 kN

Liftoff Thrust

21000 kg

LEO Capacity

GTO Capacity

Launch Record

/03
10

Total Launches

9

Successful

1

Failed

90.0%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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