Abstract: One or more electrospray emitters form an electrospray thruster, suitable for generating thrust for maneuvering and/or moving a structure to which the thruster is attached in three-dimensional space. The thruster includes a reservoir containing a fluid, preferably an ionic liquid (IL) fluid. Each electrospray emitter includes a dielectric, with channel(s) formed through a thickness thereof, and an extraction electrode, preferably an extraction grid, on an opposite side of the dielectric from the reservoir. Upon application of a sufficient electric potential differential between the extraction electrode and the fluid, the fluid flows through the channels from the reservoir, forms a Taylor cone at an outlet of each channel, and is ejected in the direction of the extraction grid to generate a thrust by the thruster for movement and/or maneuvering of the structure to which the thruster is attached.