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This Concept Map, created with IHMC CmapTools, has information related to: propulsion, cold-gas chemical propulsion Pros Simple, orbiting weight fusion rockets, H2O2 hypergolic rocket Space X: SuperDraco, Chemical Propulsion materials momentum of sunlight, restartable NO Solid fuel chemical - usually first stage rocket, Captureing / de-spin / docking requirement high specific impulse, solar sails materials propellant, liquied fuel chemcial throtlle shape / size cryogenic, restartable Candidates cold-gas chemical propulsion, xenon resource from ????, Chemical Propulsion materials propellant, Space X: SuperDraco Cons Extreme toxity, hydrazine Pros Simple, Liquid hydrogen Cons needs liquified to use, bipropellant oxidizer H2O2, Propulsion System when Near Earth Asteroid, AJ-60A Pros Cheap, Liquid oxygen Pros high performance, Near Earth Asteroid Function Main booster for low earth orbit, Atomic source radioactive materials