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This Concept Map, created with IHMC CmapTools, has information related to: Top level, Weight trades off against Redundancy, RL-10 engines utilize Cryogenic PRopellants, Vehicle design influenced by Vehicle size, Launch vehicle systems integration is dictated by Vehicle design, Propellants may be Cryogenic PRopellants, Launch vehicle systems integration requires Testing and Qualification, Propellants may be Hypergolic Propellants, Vehicle design influenced by Propellants, Launch vehicle systems integration is dictated by Engine Design, Launch vehicle systems integration requires Mechanical integration, Mechanical integration pertains to Structures, Structures significant part of Vehicle design, Redundancy ???? ????, Vehicle design illustrated by Centaur, Testing and Qualification performed on Systems, Mechanical integration pertains to Propulsion systems, Propulsion systems influenced by Vehicle size, Mechanical integration pertains to Avionics, Vehicle design influenced by Weight, Centaur powered by RL-10 engines