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Retired

Saturn IB

Saturn IB

🏭 National Aeronautics and Space Administration🌐 American📖 Wikipedia
Saturn IB

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.

21.0 t
LEO Capacity
43.2 m
Height
10
Total Launches
90.0%
Success Rate

📷 Photo Gallery

Saturn IB photo 1

📊 Specifications

📏Height
43.2 m
⭕Diameter
6.61 m
⚖️Launch Mass
590 kg
🛰️LEO Capacity
21,000 kg
🌍GTO Capacity
—
🗓️Maiden Flight
Feb 26, 1966
🚀Total Launches
10
✅Success Rate
90%
♻️Reusable
Expendable
🏭Manufacturer
National Aeronautics and Space Administration
🌐Country
American
📋Status
Retired