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Atlas V 551

Atlas V 551 is the configuration with a five-meter payload fairing, five strap-on solid rocket boosters, and a single-engine Centaur upper stage. It first flew on 2006-01-19; 23 vehicles have flown through 2026-07-02.

Atlas V 551
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Identity

Family Name
Atlas V
Full Name
Atlas V 551
Status
retired
Type
rocket
Variant Name
551

Details

Description
Atlas V 551 is the configuration with a five-meter payload fairing, five strap-on solid rocket boosters, and a single-engine Centaur upper stage. It first flew on 2006-01-19; 23 vehicles have flown through 2026-07-02.
Dimensions
Diameter M
3.81
First Flight Year
2,006
Last Flight Year
2,026
Manufacturer
Operator
Parent Vehicle Family
Propulsion Configurations
  • Entries
    • Nested value
    • Nested value
    • Nested value
    Name
    Atlas V 551 AEHF-4 propulsion
    Notes
    The AEHF-4-era 551 uses one RD-180, five Aerojet AJ-60A solid rocket boosters, and one RL10C-1 on the Centaur upper stage.
  • Entries
    • Nested value
    • Nested value
    • Nested value
    Name
    Atlas V 551 STP-3 propulsion
    Notes
    The STP-3-era 551 uses one RD-180, five GEM 63 solid rocket boosters, and one RL10C-1 on the Centaur upper stage.
Rocket Specs
Reusability
expendable
Stages Count
2

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Creation Time
July 16, 2026 at 20:38:37 UTC
Updated Time
August 1, 2026 at 07:44:21 UTC

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Atlas V 551