Some quick sims of stacked emdrives before heading out to dinner. My dims (TE311), different size holes between frustums, and far right using square waveguide.https://forum.nasaspaceflight.com/index.php?topic=37642.msg1403569#msg1403569
Nice to see a simulation of such a structure.
the waveguide including a dielectric material positioned to extend in a direction of the wave axis along a portion of the waveguide
Among all these posts about Cannae's website it is useful to remember that, since this is NASA Spaceflight.com , after alll:
1) NASA's testing of Cannae's drive that resulted in a measurable anomalous force needed the presence of a dielectric insert in the pipe connecting to the flying-saucer shaped device. There was no thrust measured by NASA without a dielectric insert in the Cannae drive.
2) NASA's computer modeling of the electric field within the pillbox and beam pipe (using COMSOL Multiphysics® software) illustrates the relative weakness of the electric field in the vicinity of the cavity slots and relative strength of the electric field within the beam pipe, especially in the drive antenna coaxial cable and the region around the cable. NASA's COMSOL analysis shows that the important part is not the flying saucer shape of the Cannae drive, but it is instead the small diameter pipe (where the dielectric insert is contained) connecting to the center of the flying-saucer shape cavity.
3) Guido Fetta's new World Patent (World Intellectual Property Organization) application Electromagnetic thrusting system WO 2016004044 A1 (Filing date Jun 30, 2015) http://www.google.com/patents/WO2016004044A1?cl=en explicitly includes a dielectric in its claims, starting with claim 1:Quotethe waveguide including a dielectric material positioned to extend in a direction of the wave axis along a portion of the waveguide
while his original US patent application Electromagnetic thruster US 20140013724 A1 (Filing date Mar 22, 2012) did not contain a reference to a dielectric insert. This inclusion of the dielectric in the patent claims follows NASA's 2014 report:
Anomalous Thrust Production from an RF Test Device Measured on a Low-Thrust Torsion Pendulum
David A. Brady*, Harold G. White†, Paul March‡, James T. Lawrence§, and Frank J. Davies
Joint Propulsion Conference
July 28-30, 2014, Cleveland, OH
AIAA 2014-4029
This material was declared a work of the U.S. Government and is not subject to copyright protection in the United States.
50th AIAA/ASME/SAE/ASEE Propulsion and Energy Forum
...
You know me by now, looking at thing a little differently and I'm looking at this differently as well.
If we are to consider the the energy within this cavity where the highest levels exist you're correct, it's in the spindle section versus the pancake section, although I would like you to consider the total amount of energy present for a the given volumes in the spindle and the pancake.
A very rough calculation is showing that >150 times greater energy levels exists per volume in the area of the pancake section versus the spindle, even though you do have a peak in the spindle area.
Food for thought.
Shell
:no dielectric = no measured anomalous force by NASA
for both completely different devices, mode shapes and natural frequencies.
no dielectric = no measured anomalous force by NASA
for both completely different devices, mode shapes and natural frequencies.
I don't mind doing some tests using HDPE. This stuff should do the trick, right?
http://www.amazon.com/dp/B000ILG0XM/ref=biss_dp_t_asn
From Cannae website: "The core of our technology uses electromagnetic, radio-frequency resonant thrusters with unique geometries creating Lorentz Force imbalances to generate thrust. Cannae has demonstrated 2 separate prototypes of a superconducting thruster which requires no dielectric material to generate thrust."
...
You know me by now, looking at thing a little differently and I'm looking at this differently as well.
If we are to consider the the energy within this cavity where the highest levels exist you're correct, it's in the spindle section versus the pancake section, although I would like you to consider the total amount of energy present for a the given volumes in the spindle and the pancake.
A very rough calculation is showing that >150 times greater energy levels exists per volume in the area of the pancake section versus the spindle, even though you do have a peak in the spindle area.
Food for thought.
Shell
1) The energy density (energy per unit volume) is higher in the pipe than in the flying-saucer shaped pillbox. Perhaps you are referring to the total energy (since there is greater volume in the flying-saucer-shaped pillbox) rather than the energy per unit volume?
2) What matters for practical purposes anyway is the anomalous force The experimental fact is simple:
no dielectric in the Cannae drive's pipe = no measured thrust by NASA
3) Cannae had to modify its patent in order to introduce the need for a dielectric (starting with claim 1), since there is no thrust without a dielectric insert
..I also find it interesting that the forces generated by the Chinese are in the same multiplier ranges as a photon rocket as the Cannae ...
no dielectric = no measured anomalous force by NASA
for both completely different devices, mode shapes and natural frequencies.
I don't mind doing some tests using HDPE. This stuff should do the trick, right?
http://www.amazon.com/dp/B000ILG0XM/ref=biss_dp_t_asn
From Cannae website: "The core of our technology uses electromagnetic, radio-frequency resonant thrusters with unique geometries creating Lorentz Force imbalances to generate thrust. Cannae has demonstrated 2 separate prototypes of a superconducting thruster which requires no dielectric material to generate thrust."
1) Thank you for asking. No, I would not use that, because the Amazon product may not be extruded. I would use an extruded HDPE big diameter rod, as used by NASA, from McMasterCarr, because rod extrusion introduces preferential alignment of the molecules (anisotropy) that may be most important in piezoelectric and other effects introduced by the dielectric
2) NASA only measured anomalous forces with the Cannae device when it had a dielectric insert. Cannae's new patent (2015) only includes a dielectric, starting in claim 1. If Cannae thinks that a dielectric is not needed, why is the dielectric now included in the claim? (why not say with a dielectric or without a dielectric?). Cannae's superconducting test results were criticized at length by zen-in.
3) Further to Cannae's experimental claims, one of their main experimental claims is that the small grooves in the flyings-saucer part of Cannae's device was most important to generate thrust, according to Cannae's computer modeling and according to their AIAA paper. However NASA showed that the Cannae grooves had practically no effect on the measurements.
..I also find it interesting that the forces generated by the Chinese are in the same multiplier ranges as a photon rocket as the Cannae ...This is not what my calculation shows. Could you please indicate the calculation for
<<the forces generated by the Chinese are in the same multiplier ranges as a photon rocket as the Cannae>> ?
Thanks
PS: Perhaps you are comparing Cannae's superconducting claims vs. Yang's not-superconducting claims?
When comparing Cannae not-superconducting to Yang's not-superconducting, then Yang's claimed force/PowerInput is much larger than Cannae's according to my calculations
..I also find it interesting that the forces generated by the Chinese are in the same multiplier ranges as a photon rocket as the Cannae ...This is not what my calculation shows. Could you please indicate the calculation for
<<the forces generated by the Chinese are in the same multiplier ranges as a photon rocket as the Cannae>> ?
Thanks
PS: Perhaps you are comparing Cannae's superconducting claims vs. Yang's not-superconducting claims?
When comparing Cannae not-superconducting to Yang's not-superconducting, then Yang's claimed force/PowerInput is much larger than Cannae's according to my calculationsForce/Power Multiple of Photon Rocket
Cannae LLC, G. Fetta, Superconducting 228400 - 285500
Chinese Non-Superconducting 270000 - 320000
Source:
http://emdrive.wiki/Experimental_Results
Both without reported dielectric inserts.
..I also find it interesting that the forces generated by the Chinese are in the same multiplier ranges as a photon rocket as the Cannae ...This is not what my calculation shows. Could you please indicate the calculation for
<<the forces generated by the Chinese are in the same multiplier ranges as a photon rocket as the Cannae>> ?
Thanks
PS: Perhaps you are comparing Cannae's superconducting claims vs. Yang's not-superconducting claims?
When comparing Cannae not-superconducting to Yang's not-superconducting, then Yang's claimed force/PowerInput is much larger than Cannae's according to my calculationsForce/Power Multiple of Photon Rocket
Cannae LLC, G. Fetta, Superconducting 228400 - 285500
Chinese Non-Superconducting 270000 - 320000
Source:
http://emdrive.wiki/Experimental_Results
Both without reported dielectric inserts.
But the quoted test for Yang is not-superconducting, while the test for Cannae is superconductiing.
Superconductivity severely affects the conductivity of the metal and hence severely affects the quality of resonance Q.
I think it would be more appropriate to compare Cannae's tests with not superconducting material with Yang's tests.
Rigid HDPE Polyethylene Rod, 6" Diameter
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Rigid HDPE Polyethylene Rod, 6" Diameter
More About Plastics
Length, ft.
1
Each
ADD TO ORDER
In stock
$70.39 Each
McMaster is located here in Atlanta. How convenient! I think NASA used two of the 6" diameter 1" length discs that run $18.54 each: http://www.mcmaster.com/#hdpe/=11zr8dk
I do not think I can get a 6" disc through the small end opening of my frustum, so I may have to go with the 4 or 5 inch. Does this stuff bend or is it very rigid like resin? If i can double it over I won't have to cut each disk in half.
Dr, Rodal,
It maybe appropriate to review this as it's interesting that three things are apparent.
1. Vastly different drive shapes and configurations and both reported thrust.
2. Neither reported using dielectrics.
3. One was superconducting and the other not.
Shell
Dr, Rodal,
It maybe appropriate to review this as it's interesting that three things are apparent.
1. Vastly different drive shapes and configurations and both reported thrust.
2. Neither reported using dielectrics.
3. One was superconducting and the other not.
ShellIt is also appropriate to consider the following experimental results and patents in such a review:
How should we interpret/analyze the reported experimental result that NASA only measured anomalous thrust for the Cannae non-superconducting device when introducing a dielectric insert in the Cannae pipe ?
And the fact that Cannae, after NASA's 2014 measurement, incorporated a dielectric in Cannae's 2015 patent claims?
Dr, Rodal,
It maybe appropriate to review this as it's interesting that three things are apparent.
1. Vastly different drive shapes and configurations and both reported thrust.
2. Neither reported using dielectrics.
3. One was superconducting and the other not.
ShellIt is also appropriate to consider the following experimental results and patents in such a review:
How should we interpret/analyze the reported experimental result that NASA only measured anomalous thrust for the Cannae non-superconducting device when introducing a dielectric insert in the Cannae pipe ?
And the fact that Cannae, after NASA's 2014 measurement, incorporated a dielectric in Cannae's 2015 patent claims?
I do not think we should take seriously NASA's measurements with/without dielectric inserts. Was in one measurement the cannie drive grounded, and in another measurement not grounded? If in one measurement the drive was grounded, what was the shape of the RF cable in that measurement? These were factors that could have dramatically changed the Lorentz forces in their measurements, which had the same size as their measured thrust. Since they did not consider the Lorentz forces, their measurements were not valid and no conclusion should be drawn from their measurements.
Rigid HDPE Polyethylene Rod, 6" Diameter
More About Plastics
Length, ft.
1
Each
ADD TO ORDER
In stock
$70.39 Each
McMaster is located here in Atlanta. How convenient! I think NASA used two of the 6" diameter 1" length discs that run $18.54 each: http://www.mcmaster.com/#hdpe/=11zr8dk
I do not think I can get a 6" disc through the small end opening of my frustum, so I may have to go with the 4 or 5 inch. Does this stuff bend or is it very rigid like resin? If i can double it over I won't have to cut each disk in half.