Micropropulsion: Investigation of Alternative Propulsion Concepts
|Principal investigator:||John STARK|
|Co-investigator(s):||K.L. Smith, M.S.. Alexander and M.D. Paine|
|Funding source(s):||Commission of the European Community|
|Start: 01-12-2010 / End: 30-11-2013|
The colloid thruster uses electrospray atomization, whereby an electrolytic fluid (with conductivity ~1S/m) is injected, from an emitter, into an electric field (~1kV/mm) generated by an electrical potential difference between the emitter and an extraction grid. The fluid, under the influence of the electric field, forms a structure known as a Taylor cone. At the apex of this cone a jet is formed which subsequently breaks up to form a charged spray with species having a charge to mass ratio, q/m, typically 1-100kC/kg. This charged spray is then accelerated in a static electric field to produce a thrust. Figure 1 shows images of these cone-jet structures formed on micro-fabricated arrays .
A schematic of a typical configuration is given in Figure 2.
This research is funded by the European Space Agency (ESA). ESA Programme manager Dr Clive Edwards