Emission Characteristics of Passively Fed Electrospray Microthrusters with Propellant Reservoirs-Reference-Cited by-同舟云学术

Emission Characteristics of Passively Fed Electrospray Microthrusters with Propellant Reservoirs

Published:2017-03 Issue:2 Volume:54 Page:447-458
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Krejci David,Mier-Hicks Fernando,Thomas Robert,Haag Thomas,Lozano Paulo¹

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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