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.