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Hardware/Vehicles/Atlas Centaur

Atlas Centaur

Retired

General Dynamics (Convair) · 2-stage orbital rocket · Part of the Atlas family

Total Launches
0
Success Rate
—
Payload to LEO
—
First Flight
1962
Reusable
No

Specifications

Height33 m
Diameter3.05 m
Wet Mass136,100 kg
Payload to GTO1.7 t
Payload to SSON/A
ManufacturerGeneral Dynamics (Convair)
CountryUnited States

Engines Used

No engine records tracked for this vehicle yet.

    Engine usage data lives in the Engine Dashboard.

    Launch History

    No launches attributed to this vehicle in the database yet.

    Reliability by Year

    Reliability data not available yet.

    Related Entities

    Atlas IVehicle familyAtlas IIVehicle familyAtlas IIAVehicle familyAtlas IIASVehicle familyAtlas 3AVehicle familyAtlas 3BVehicle family

    Data Sources for This Record

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