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Atlas III launch vehicle family

Atlas III was Lockheed Martin's transitional Atlas-Centaur generation. It replaced the classic booster-and-sustainer propulsion package with one Russian-built RD-180 while retaining pressure-stabilized Atlas propellant tanks. Two IIIA and four IIIB vehicles completed six successful missions from 2000 through 2005, introducing the RD-180 and stretched Centaur architecture carried into Atlas V.

Atlas III launch vehicle family
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Identity

Aliases
Atlas III seriesAtlas III-Centaur family
Family Name
Atlas III
Full Name
Atlas III launch vehicle family
Status
retired
Type
rocket

Details

Description
Atlas III was Lockheed Martin's transitional Atlas-Centaur generation. It replaced the classic booster-and-sustainer propulsion package with one Russian-built RD-180 while retaining pressure-stabilized Atlas propellant tanks. Two IIIA and four IIIB vehicles completed six successful missions from 2000 through 2005, introducing the RD-180 and stretched Centaur architecture carried into Atlas V.
First Flight Year
2,000
Last Flight Year
2,005
Manufacturer
Operator
Parent Vehicle Family
Propulsion Configurations
  • Entries
    • Count
      1
      Placement
      core
      Propulsion System
      Role
      main
      Stage
      first-stage
      Variant Notes
      One exact RD-180 on the Atlas III redesigned first stage.
    • Count
      1
      Placement
      upper
      Propulsion System
      Role
      upper-stage
      Stage
      second-stage
      Variant Notes
      One exact RL10A-4-1B on the Atlas IIIA single-engine Centaur.
    Name
    Atlas IIIA
    Notes
    Atlas IIIA configuration: one RD-180 on the redesigned booster and one RL10A-4-1B on the single-engine Centaur upper stage.
  • Entries
    • Count
      1
      Placement
      core
      Propulsion System
      Role
      main
      Stage
      first-stage
      Variant Notes
      One exact RD-180 on the Atlas III redesigned first stage.
    • Count
      1
      Placement
      upper
      Propulsion System
      Role
      upper-stage
      Stage
      second-stage
      Variant Notes
      One exact RL10A-4-1B on the Atlas IIIB single-engine Common Centaur option.
    Name
    Atlas IIIB (single-engine Centaur)
    Notes
    Atlas IIIB single-engine Centaur option: the Atlas III RD-180 booster with one RL10A-4-1B on the stretched Centaur upper stage.
  • Entries
    • Count
      1
      Placement
      core
      Propulsion System
      Role
      main
      Stage
      first-stage
      Variant Notes
      One exact RD-180 on the Atlas III redesigned first stage.
    • Count
      2
      Placement
      upper
      Propulsion System
      Role
      upper-stage
      Stage
      second-stage
      Variant Notes
      Two exact RL10A-4-1B engines on the Atlas IIIB dual-engine Common Centaur option.
    Name
    Atlas IIIB (dual-engine Centaur)
    Notes
    Atlas IIIB dual-engine Centaur option: the Atlas III RD-180 booster with two RL10A-4-1B engines on the stretched Centaur upper stage.
Rocket Specs
Reusability
expendable
Stages Count
2

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Creation Time
July 14, 2026 at 06:51:57 UTC
Updated Time
August 1, 2026 at 13:49:20 UTC