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Tag Archives: Aerojet
Dual Propellant Expander
Or what you are going to call it, an unrealized proposal from Aerojet around 1984. PDF Found on NTRS. The idea was to have two turbopumps (like on SSME), but instead operate on the expander cycle. Two heat exchangers, two … Continue reading →
Posted in Architecture, Depot, engines, industry, ISRU, Lunar, NASA, RLV:s, Spacecraft, Transportation
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Tagged Aerojet, Expander, Hydrogen, LOX
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