Figure 26 shows the dielectric they plan for their next generation RF thruster. It looks to me like it fills the cavity completely. I can't guess how much room there will be for air. Not much?
1) The
dielectric resonators must have been responsible for the NASA-measured thrust forces, for both the Cannae and the Frustum devices, as
when they removed the dielectric resonators from either of them, they could not measure any thrust. 2) The calculated Electric Field in the dielectric resonators is much, much stronger than in the rest of the cavity.
3) The
volumes of the dielectric resonators are significantly smaller than the total inner
volumes of the cavities. One can assess the dielectric resonators relative size and location from Fig. 14, p.10, as the dielectric resonator appears red (in the Electric Field calculation display) surrounded by a narrow amount of yellow and a lot of blue. Fig. 14 shows the PTFE (Teflon) dielectric resonator for the Cannae device. It appears to have a cylindrical shape (small diameter/length ratio). Fig. 26, p.21 showing the "Next Generation RF [Frustum] Thruster" shows an annular-shaped (a disc with an inner hole) dielectric resonator. Yes, the annular-shaped dielectric resonator takes a significant amount of the
area at the small diameter end of the Frustum, but it takes a rather insignificant amount of the total
volume inside the cavity.
4) Notice the very
un-symmetric location of the dielectric resonators. For both the Cannae and the Frustum devices, the dielectric resonators are located towards one end of the device. The direction of measured thrust is the same as the relative location of the dielectric resonator. Defining "left" and "right" in fixed-in-space extrinsic coordinates: with the dielectric resonator located towards the right of the device's center of mass, thrust occurred towards the right. When the device was turned around by 180 degrees such that the dielectric resonator was located towards the left of the center of mass, thrust occurred towards the left.
5) The picture of the Frustum seems to show a diameter ratio ( (large diameter)/(small diameter) ) = 1.71 instead of the guesstimated ratio ( (large diameter)/(small diameter) ) = 9.9"/6.6" = 1.50 based on the photograph and the cross-section of the Faztek beam. Also the picture seems to show a ( (large diameter)/(length) ) = 1.20 instead of the guesstimated ratio ( (large diameter)/(length) ) = 9.9"/9.0" = 1.10, and ( (length)/( small diameter) ) = 1.43 instead of the guesstimated ratio ( (length)/( small diameter) ) = 9.0"/6.6" = 1.36. Therefore the ratios I guesstimate from this picture, divided by your guesstimated ratios are: 1.14, 1.09 and 1.05 respectively. The differences are relatively small, the maximum difference being for the diameter ratio (14% difference between our estimates) and the smallest difference being for the estimation of the ( (length)/( small diameter) ) ratio (5% difference between our estimates). In any case, please double-check these dimensional ratios and let us know what you think.
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Images from "Anomalous Thrust Production from an RF Test Device Measured on a Low-Thrust Torsion Pendulum" by David A. Brady*, Harold G. White†, Paul March‡, James T. Lawrence§, and Frank J. Davies**, July 28-30, 2014, Cleveland, OH, AIAA 2014-4029, Propulsion and Energy Forum, 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
the article notes: "This material is declared a work of the U.S. Government and is not subject to copyright protection in the United States." (Also see:
http://en.wikipedia.org/wiki/Copyright_status_of_work_by_the_U.S._government) as posted in
http://www.libertariannews.org/wp-content/uploads/2014/07/AnomalousThrustProductionFromanRFTestDevice-BradyEtAl.pdf