DBSE
Hardware/Vehicles/Saturn I

Saturn I

Retired

NASA / MSFC · 3-stage orbital rocket · Part of the Saturn family

Total Launches
6
Success Rate
100%
Payload to LEO
9 t
First Flight
1961
Reusable
No

Interactive Model

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Specifications

Height50.4 m
Diameter6.6 m
Wet Mass420,000 kg
Payload to GTON/A
Payload to SSON/A
ManufacturerNASA / MSFC
CountryUnited States

Engines Used

No engine records tracked for this vehicle yet.

    Engine usage data lives in the Engine Dashboard.

    Launch History

    Reliability by Year

    Related Entities

    Saturn IBVehicle familyNASA / MSFCManufacturer

    Data Sources for This Record

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