Design and analysis of MEMS based electrospray thruster

Author:

Rao K. SrinivasaORCID,Kumar Y. Sundar Sai,Rohini K. Sai Sree,Ravi P.,Sravani K. G.,Kumar P. Ashok

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Hardware and Architecture,Condensed Matter Physics,Electronic, Optical and Magnetic Materials

Reference39 articles.

1. Alyssa R, Jason AY, Andrea GH, Thomas JC. Characterization of a single emitter electrospray thruster. Research Gate. https://doi.org/10.13140/rg.2.2.28585.24165

2. Chakraborty S, Ataman C, Dandavino S, Shea H (2012) Microfabrication of an electrospray thruster for small spacecraft. Power MEMS

3. Chiu Y, Dressler RA (2007) Ionic liquids for space propulsion. Ionic Liquids IV 138:160. https://doi.org/10.1021/bk-2007-0975.ch010

4. Coffman CS (2016) Electrically-assisted evaporation of charged fluids: Fundamental modeling and studies on ionic liquids (Doctoral dissertation, Massachusetts Institute of Technology)

5. Courtney D, Lozano P (2009) Development of ionic liquid electrospray thrusters using porous emitter substrates. International Conference on Space Technology and Science, pp 1–6

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