Emission Characteristics of Passively Fed Electrospray Microthrusters with Propellant Reservoirs
Author:
Affiliation:
1. Massachusetts Institute of Technology, Cambridge, Massachusetts 02139
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A33531
Reference36 articles.
1. A survey and assessment of the capabilities of Cubesats for Earth observation
2. Electrospray as a Source of Nanoparticles for Efficient Colloid Thrusters
3. Carretero BenignosJ. “Numerical Simulation of a Single Emitter Colloid Thruster in Pure Droplet Cone-Jet Mode,” Ph.D. Dissertation, Massachusetts Inst. of Technology, Cambridge, MA, 2005.
4. Experimental measurements of Colloid Thruster plumes in the ion-droplet mixed regime
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