Emission Characteristics of Passively Fed Electrospray Microthrusters with Propellant Reservoirs
The characterization of a miniaturized ionic liquid electrospray thruster for nanosatellite applications is presented. The thruster investigated features an emitter array of 480 emitter tips per square centimeter and a 1 cm[superscript 3] propellant tank with an entirely passive propellant supply;...
| Main Authors: | , , , , |
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| Other Authors: | |
| Format: | Article |
| Language: | en_US |
| Published: |
American Institute of Aeronautics and Astronautics
2017
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| Online Access: | http://hdl.handle.net/1721.1/108538 https://orcid.org/0000-0003-4278-8951 https://orcid.org/0000-0003-1648-0902 https://orcid.org/0000-0002-6063-3227 |