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Atlas II

The baseline Atlas II increased Atlas-Centaur performance for Defense Satellite Communications System, UHF Follow-On, and commercial payloads. Its pressure-stabilized Atlas stage used the MA-5A propulsion system and fed a two-engine Centaur II. Ten vehicles flew successfully from Eutelsat II F3 in December 1991 through UHF F8 in March 1998.

Atlas II
NASA/Bill Ingalls · Stored/public JPEG is byte-identical to the NASA canonical 201108050008HQ large asset (1279x1920, SHA-256 54592683e90ae091eefed5173f1276a07ae2326599475516c32c208dbfd60e1c). NASA Images API metadata identifies the exact image as Atlas V Rocket Launches with Juno Spacecraft, photographed by NASA/Bill Ingalls, and describes the Atlas V/Juno launch from Space Launch Complex 41 on August 5, 2011. NASA current Images and Media Usage Guidelines state that NASA content may be used factually or informationally with NASA acknowledged, while NASA-hosted third-party content is marked and NASA use does not convey rights; commercial use must not imply endorsement and NASA logos and identifiers remain protected: https://www.nasa.gov/nasa-brand-center/images-and-media/. This is an asset-level, conservative factual/editorial reuse basis with NASA/Bill Ingalls attribution, not a blanket license for promotional content, merchandise, NASA branding, or endorsement. · Source
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Identity

Aliases
Atlas II-CentaurAtlas II/CentaurBaseline Atlas II
Family Name
Atlas II
Full Name
Atlas II
Status
retired
Type
rocket
Variant Name
II

Details

Description
The baseline Atlas II increased Atlas-Centaur performance for Defense Satellite Communications System, UHF Follow-On, and commercial payloads. Its pressure-stabilized Atlas stage used the MA-5A propulsion system and fed a two-engine Centaur II. Ten vehicles flew successfully from Eutelsat II F3 in December 1991 through UHF F8 in March 1998.
Dimensions
Diameter M
3.05
Height M
47.5
First Flight Year
1,991
Last Flight Year
1,998
Manufacturer
Parent Vehicle Family
Propulsion Configurations
  • Entries
    • Nested value
    • Nested value
    • Nested value
Rocket Specs
Liftoff Mass Kg
187,600
Payload Capacity Kg
Gto
2,810
Leo
6,580
Reusability
expendable
Stages Count
2
Strap On Boosters Count
0

Links

Official Url
https://www.nasa.gov/wp-content/uploads/2023/04/sp-4012v7.pdf

Assets & Meta

Creation Time
July 14, 2026 at 06:51:40 UTC
Updated Time
July 29, 2026 at 15:34:59 UTC
Image
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Search Name
Atlas II Atlas II-Centaur Atlas II/Centaur Baseline Atlas II