Caballero-Pérez et al., 2022 - Google Patents
Effect of operating variables on the propulsive performance of cone-jet electrospraysCaballero-Pérez et al., 2022
View PDF- Document ID
- 3192596762316851367
- Author
- Caballero-Pérez M
- Gamero-Castaño M
- Publication year
- Publication venue
- 37th International Electric Propulsion Conference, Cambridge, Massachusetts
External Links
Snippet
Electrospray thrusters are a promising form of propulsion that have been proposed as the primary propulsion system for small satellites and attitude control for larger spacecraft. Electrospray describes the atomization process of a liquid subjected to an intense electric …
- 230000000694 effects 0 title description 11
Classifications
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- H—ELECTRICITY
- H01—BASIC ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J49/00—Particle spectrometer or separator tubes
- H01J49/02—Details
- H01J49/10—Ion sources; Ion guns
- H01J49/16—Ion sources; Ion guns using surface ionisation, e.g. field-, thermionic- or photo-emission
- H01J49/165—Electrospray ionisation
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- H—ELECTRICITY
- H01—BASIC ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J49/00—Particle spectrometer or separator tubes
- H01J49/02—Details
- H01J49/04—Arrangements for introducing or extracting samples to be analysed, e.g. vacuum locks; Arrangements for external adjustment of electron- or ion-optical components
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