DBSE
Hardware/Vehicles/Saturn IB

Saturn IB

Retired

NASA / MSFC · 2-stage orbital rocket · Part of the Saturn family

Total Launches
8
Success Rate
87.5%
Payload to LEO
—
First Flight
1966
Reusable
No

Interactive Model

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Specifications

Height68.1 m
Diameter6.53 m
Wet Mass587,300 kg
Payload to GTON/A
Payload to SSON/A
ManufacturerNASA / MSFC
CountryUnited States

Engines Used

Engine usage data lives in the Engine Dashboard.

Launch History

Reliability by Year

Related Entities

Saturn IVehicle familyNASA / MSFCManufacturerJ-2Engine

Data Sources for This Record

Specifications
GCAT / Wikipedia · verified quarterly
Launch History
LL2 API · updated every 6h
Engine Data
Manufacturer + Wikidata