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NASA NTRS ยท 20010125606

Apparatus and Method for Generating Thrust Using a Two Dimensional, Asymmetrical Capacitor Module

Abstract

A capacitor module system is provided for creating a thrust force. The system includes a capacitor module provided with a first conductive element having a cylindrical geometry. The first conductive element can be a hollow cylinder or a solid cylinder. The capacitor module also includes a second conductive element axially spaced from the first conductive element and of smaller axial extent. The second conductive element can be a flat disk, a dome, or a conductive tip at the end of a dielectric rod. A dielectric element is disposed between the first conductive element and the second conductive element. The system also includes a high voltage source having first and second terminals connected respectively to the first and second conductive elements. The high voltage source applies a high voltage to the conductive elements of sufficient value to create a thrust force on the module inducing movement thereof.

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BibTeXRIS

Jonathan W Campbell. 2001-11-13. Apparatus and Method for Generating Thrust Using a Two Dimensional, Asymmetrical Capacitor Module. https://ntrs.nasa.gov/citations/20010125606

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