A propulsion apparatus for space vehicles, includes a solid state oxygen-rich source layer, means for extracting oxygen from said solid state oxygen-rich source layer, means for accelerating correspondingly extracted oxygen ions into vacuum. A stack includes the solid state oxygen-rich source layer, an active layer being deposited above the solid state oxygen-rich source layer, in contact with the solid state oxygen rich source layer, the active layer being formed with a material different from the solid state oxygen-rich source layer, the material being an oxide presenting impedance hysteresis behavior.
PROPULSION APPARATUS FOR SPACE VEHICLES AND CORRESPONDING METHOD / Chiolerio, A.; Porro, S.. - (2016).
Titolo: | PROPULSION APPARATUS FOR SPACE VEHICLES AND CORRESPONDING METHOD |
Autori: | |
Data di pubblicazione: | 2016 |
Abstract: | A propulsion apparatus for space vehicles, includes a solid state oxygen-rich source layer, means for extracting oxygen from said solid state oxygen-rich source layer, means for accelerating correspondingly extracted oxygen ions into vacuum. A stack includes the solid state oxygen-rich source layer, an active layer being deposited above the solid state oxygen-rich source layer, in contact with the solid state oxygen rich source layer, the active layer being formed with a material different from the solid state oxygen-rich source layer, the material being an oxide presenting impedance hysteresis behavior. |
Appare nelle tipologie: | 6.1 Brevetto |
File in questo prodotto:
File | Descrizione | Tipologia | Licenza | |
---|---|---|---|---|
US20200277088A1.pdf | 2a Post-print versione editoriale / Version of Record | PUBBLICO - Tutti i diritti riservati | Visibile a tuttiVisualizza/Apri |
http://hdl.handle.net/11583/2847398