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Aerojet YLR-91-AJ-7

Historical Aerojet-General YLR-91-AJ-7 storable bipropellant second-stage engine for the Titan II Gemini Launch Vehicle. NASA identifies the YLR-91-AJ-7 as the GLV Stage II engine, and NASA dates Gemini I's first production Titan II launch to 1964-04-08; this record uses that date as the engine assembly's first flight. NASA's Gemini-Titan table lists one YLR-91-AJ-7 engine at 100,000 lbf (about 444.8 kN) sea-level thrust, using UDMH and nitrogen tetroxide as the single second-stage powerplant.

Identity

Aliases
YLR91-AJ-7
Domains
spaceflight
Identity Level
variant
Kind
liquid-rocket-engine
Name
Aerojet YLR-91-AJ-7
Status
historical

Details

Description
Historical Aerojet-General YLR-91-AJ-7 storable bipropellant second-stage engine for the Titan II Gemini Launch Vehicle. NASA identifies the YLR-91-AJ-7 as the GLV Stage II engine, and NASA dates Gemini I's first production Titan II launch to 1964-04-08; this record uses that date as the engine assembly's first flight. NASA's Gemini-Titan table lists one YLR-91-AJ-7 engine at 100,000 lbf (about 444.8 kN) sea-level thrust, using UDMH and nitrogen tetroxide as the single second-stage powerplant.
Developers
First Flight Date
1964-04-08
Manufacturers
Propellants
UDMHnitrogen tetroxide
Rocket Specs
Sea Level Thrust Kn
444.8

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Assets & Meta

Creation Time
July 29, 2026 at 08:15:42 UTC
Updated Time
August 22, 2026 at 11:01:30 UTC

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