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AJ26

AJ26 is Aerojet's modified Russian NK-33 configuration used as a pair on the retired Antares 100-series first stage. NASA documents the conversion boundary for U.S. launch-vehicle use and lists approximately 338,000 lbf (1,505 kN) thrust for the Antares application; the existing direct-derivative lineage and retired status are preserved.

AJ26
NASA · Public domain in the United States; the Commons record identifies NASA as author and the image as solely created by NASA. Preserve NASA attribution and do not imply NASA endorsement; NASA logos and emblems remain separately restricted. · Source

Identity

Domains
spaceflight
Identity Level
model
Kind
liquid-rocket-engine
Name
AJ26
Status
retired

Details

Description
AJ26 is Aerojet's modified Russian NK-33 configuration used as a pair on the retired Antares 100-series first stage. NASA documents the conversion boundary for U.S. launch-vehicle use and lists approximately 338,000 lbf (1,505 kN) thrust for the Antares application; the existing direct-derivative lineage and retired status are preserved.
Developers
Lineage
  • Note
    NASA's investigation identifies AJ26 as an NK-33 core modified by Aerojet for U.S. launch-vehicle use.
    Related Propulsion System
    Relationship
    direct-derivative-of
    Sources
Manufacturers
Propellants
RP-1liquid oxygen
Rocket Specs
Sea Level Thrust Kn
1,505

Links

Assets & Meta

Creation Time
July 29, 2026 at 08:15:51 UTC
Updated Time
August 22, 2026 at 07:00:23 UTC

Other

Sources
AJ26 - AeroVia