WARNING:
JavaScript is turned OFF. None of the links on this concept map will
work until it is reactivated.
If you need help turning JavaScript On, click here.
This Concept Map, created with IHMC CmapTools, has information related to: Propulsionv2.cmap, Chemical rockets Are fueled by In Situ Resources, Propulsion Can utilize SEP, Achieve Earth orbit Consists of Multi Stage, Hall/ion thrusters but are Power limited, Power limited which requires Large solar arrays, Nuclear thermal, Single stage which are Low TRL, Large solar arrays, Nuclear thermal for Accelerated mission times, Propulsion Consists of Chemical rockets, Propulsion Depends on Mission Duration, Electromagnetic options but are Power limited, Propulsion Depends on Mission Goals, Propulsion Depends on Distance Traveled, Multi Stage which are inefficient, SEP only for Orbital maneuvers, Multi Stage which are Non-reusable, Chemical rockets to Change attitude, Multi Stage which are Expensive, Propulsion Depends on Mission Payload, Chemical rockets Are fueled by Carry on sources, Single stage which are Reusable