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Consuming long-range interplanetary medium with fuel for driving plasmathrust is vital. Methods of capturing the space environment depending on itsdensity and the ship velocity are indispensable issues to extract the spaceenvironment as a propellant. This matter of neutral fluxes would use solarradiation to create ionization in a plasma thruster. Extracting propellant atcertain ranges look extremely promising where a low thrust device operatescontinuously to deliver a celestial target close at the speed of light.However, at longer distances, the density of space rapidly diminishes and itmay be impossible to maintain at a plasma thruster continuous operation modebut instead might be workable with a pulsed engine. Nonetheless, at stilllonger-range interstellar missions, the insufficient propellant will requireexamining other alternatives than a plasma thruster for other candidatepropulsion system, possibly either propellantless or a propulsor is driven byelectric and/or magnetic fields to satisfy these mission objectives.

Using Interplanetary Medium as Propellant for Plasma Thruster Propulsion