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This Concept Map, created with IHMC CmapTools, has information related to: ARM Basic Concepts, Asteroid Characterization to determine Asteroid Dynamics, Redirect ending with Human Exploration, Solar Electric Propulsion operating at 40 kW, Search for Suitable Asteroid followed by Rendezvous, Asteroid Dynamics may require Despin, Asteroid Characterization followed by Approach and Capture, Search for Suitable Asteroid with acceptable Composition, Approach and Capture followed by Redirect, Redirect to achieve Distant Retrograde Lunar Orbit, Search for Suitable Asteroid with acceptable Spin, Rendezvous followed by Asteroid Characterization, Search for Suitable Asteroid with acceptable Orbit, Rendezvous accomplished using Solar Electric Propulsion, Asteroid Redirect Mission begins with Search for Suitable Asteroid, Approach and Capture accomplished using inflatable capture bag, Search for Suitable Asteroid with acceptable Size