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Aerojet AJ10-138 rocket engine

Aerojet's historical AJ10-138 was a pressure-fed, restartable storable-propellant engine used in Titan Transtage propulsion and adapted for Voyager work. NASA documents nitrogen tetroxide/Aerozine-50 propellants, multiple zero-gravity restarts, and two AJ10-138 engines mounted on a common Transtage frame producing 16,000 lbf combined vacuum thrust; this record does not collapse the two-engine installation into a single-engine performance claim.

Identity

Aliases
AJ10-138AJ 10-138AJ10-138 Transtage engine
Domains
spaceflight
Identity Level
model
Kind
liquid-rocket-engine
Name
Aerojet AJ10-138 rocket engine
Status
historical

Details

Description
Aerojet's historical AJ10-138 was a pressure-fed, restartable storable-propellant engine used in Titan Transtage propulsion and adapted for Voyager work. NASA documents nitrogen tetroxide/Aerozine-50 propellants, multiple zero-gravity restarts, and two AJ10-138 engines mounted on a common Transtage frame producing 16,000 lbf combined vacuum thrust; this record does not collapse the two-engine installation into a single-engine performance claim.
Propellants
nitrogen tetroxideAerozine-50
Rocket Specs
Cycle
pressure-fed
Restartable
Yes

Links

Assets & Meta

Creation Time
August 15, 2026 at 05:34:44 UTC
Updated Time
August 15, 2026 at 05:34:44 UTC

Other

Sources
  • Accessed Date
    2026-08-14
    Note
    NASA's Voyager Transtage study identifies two unmodified pressure-fed fixed-thrust AJ10-138 engines, their common-frame installation, combined 16,000 lbf vacuum thrust, and multiple zero-gravity restarts.
    Publisher
    NASA Technical Reports Server
    Title
    Voyager Spacecraft System Final Report
  • Accessed Date
    2026-08-14
    Note
    NASA's Titan III propulsion analysis identifies the Transtage as two AJ10-138 engines working in tandem and distinguishes their pressure-fed storable-liquid architecture from the LR87/LR91 stage engines.
    Publisher
    NASA Technical Reports Server
    Title
    Titan III Propulsion Systems