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Hardware/Vehicles/Atlas IIAS

Atlas IIAS

Retired

Lockheed Martin · 2-stage orbital rocket · Part of the Atlas family

Total Launches
30
Success Rate
100%
Payload to LEO
8.6 t
First Flight
1993
Reusable
No

Specifications

Height47.4 m
Diameter3.05 m
Wet Mass237,200 kg
Payload to GTO3.7 t
Payload to SSON/A
ManufacturerLockheed Martin
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

    Atlas CentaurVehicle familyAtlas IVehicle familyAtlas IIVehicle familyAtlas IIAVehicle familyAtlas 3AVehicle familyAtlas 3BVehicle familyLockheed MartinManufacturer

    Data Sources for This Record

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