The studies were made considering a continuous beam of photons being reflected inside a truncated cone cavity.
Great work! Two things: 1. Can you fun the simulation for a truncated cone with rounded endplates with the same center radius? 2. Suggest also running the simulation with the laser firing less randomly and more like the angle shown in this image.
Dr. Rodal, thank you for your reply! Re the NASA frustum is there an ideal location for exciting TE012?, and would going with a larger frustum (say x2 larger), with a much higher Q, help in "locking down" the mode? FL
...here the maximum Blongitudinal field intensity occurs, to try to excite the axial magnetic field that takes place in the longitudinal direction with a TE mode. ...
...here the maximum Blongitudinal field intensity occurs, to try to excite the axial magnetic field that takes place in the longitudinal direction with a TE mode. ...
So this image of the antenna here would be the optimal location to excite the TE012 mode? Am I right that the loop perimeter is half the wavelength of the current in the wire? Wires twisted when not in loop to eliminate B field generation. Image from Dr. Rodals pic of TE012, screen shot, then doodled over in paint.
My studies on the EmDrive based on Ray Tracing is done, paper is attached.
In paper it is described how the algorithm was made, and it is discussed some results obtained for some cases.
I'm running some simulations now with higher number of iterations (reflections), but it will take a longer time to get the results. Still with some issues with preallocating memory on the algorithm.
The studies were made considering a continuous beam of photons being reflected inside a truncated cone cavity.
The asymmetry of the cone geometry causes an imbalance in the angle of incidence between the two ends, which I believe is the main cause for the resulting net thust. Calculations with a geometry of a cylinder resulted in zero thrust.
Thrust is towards small end.

Just my luck. The RF Instruments spectrum analyser sold out just one hour before I whipped out my credit card to make the purchase. I have an email into them to see when another batch will be ready.
http://www.ebay.com/itm/USB-RF-Spectrum-Analyzer-3-3GHZ-/282009631423
Just my luck. The RF Instruments spectrum analyser sold out just one hour before I whipped out my credit card to make the purchase. I have an email into them to see when another batch will be ready.
http://www.ebay.com/itm/USB-RF-Spectrum-Analyzer-3-3GHZ-/282009631423http://www.hamradio.com/detail.cfm?pid=H0-013596
Maybe look here, where I got mine.
Shell
Your results (a thrust force for a given amount of input power, in excess of a perfect photon rocket) clearly violate both conservation of momentum and conservation of energy.
Your solution depends on a large number of numerical calculations with finite precision. Due to round-off conservation of momentum and energy may be lost in each calculation.
It would be more convincing if conservation of momentum and energy would be enforced by a side-condition, after every few calculations.
The first thing I would look to is the conditioning of your solution matrix. Is it ill-conditioned? Have you looked at the relative size of all its diagonal members?
What is the value of
for your solution matrix throughout the calculations?
Can you plot kappa from the first calculation to the end ? What does it look like?
Your results (a thrust force for a given amount of input power, in excess of a perfect photon rocket) clearly violate both conservation of momentum and conservation of energy.
What about the conservation of momentum and the thrust measured in EmDrive experiments?
For a given cavity dimension and beam initial trajectory, there must be a certain number of reflections until the "path loop" is closed so the thrust returns to zero, keeping the conservation of momentum.
Image attached shows a case where thrust has returned to zero after approximately 110,000 reflections:
This means that for a beam being continuously reflected inside a cavity, thrust would be cyclic, and returns to zero every time the path loop for conservation of momentum is closed. But, if a beam is reflected and absorbed before the path loop is closed, net thrust is observed.
Yet this does not explain thrust higher than a photon rocket of same power.
I've checked the equations in the algorithm, everything seems right.Your solution depends on a large number of numerical calculations with finite precision. Due to round-off conservation of momentum and energy may be lost in each calculation.
Cylinder case is still giving zero thrust after 250,000 iterations, as expected, I have checked the resulting thrust variable value, absolute zero, round-off is not being a problem.It would be more convincing if conservation of momentum and energy would be enforced by a side-condition, after every few calculations.
The first thing I would look to is the conditioning of your solution matrix. Is it ill-conditioned? Have you looked at the relative size of all its diagonal members?
What is the value of
for your solution matrix throughout the calculations?
Can you plot kappa from the first calculation to the end ? What does it look like?
I will look into it.
Thanks for your notes Dr. Rodal.

Dr. Rodal, at the end of the Ames talk Sonny describes moving forward and mentions "phase lock loop", forgive my high school physics only, but would phase lock looping eliminate or mitigate the issues associated with modes being "close" to one another? Not to mention your above mentioned antenna looping and position. Your help is greatly appreciated. FL (below attached image of "moving forward" frustum)
My studies on the EmDrive based on Ray Tracing is done, paper is attached.
In paper it is described how the algorithm was made, and it is discussed some results obtained for some cases.
...
My studies on the EmDrive based on Ray Tracing is done, paper is attached.
In paper it is described how the algorithm was made, and it is discussed some results obtained for some cases.
...Thank you for posting this paper.
I started going through your equations and found an issue with your definition of the normal vector for the sidewalls.
I believe the correct expression should be
[-x/R * cos(Φ) , -y/R * cos(Φ), sin(Φ)]
This expression is also written in a form that should always be normalized as long as x^2 +y^2 = R^2.
The mistake vanishes when Φ = 0, explaining why you got the expected result for a cylinder. This flows into your other calculations, so I will let you correct this before I review the other technical details more thoroughly.
Dr. Rodal, at the end of the Ames talk Sonny describes moving forward and mentions "phase lock loop", forgive my high school physics only, but would phase lock looping eliminate or mitigate the issues associated with modes being too "close" to one another? Not to mention your above mentioned antenna looping and positioning advice. Your help is greatly appreciated. FL (below attached image of "moving forward" frustum)

Dr. Rodal, at the end of the Ames talk Sonny describes moving forward and mentions "phase lock loop", forgive my high school physics only, but would phase lock looping eliminate or mitigate the issues associated with modes being too "close" to one another? Not to mention your above mentioned antenna looping and positioning advice. Your help is greatly appreciated. FL (below attached image of "moving forward" frustum)
My studies on the EmDrive based on Ray Tracing is done, paper is attached.
In paper it is described how the algorithm was made, and it is discussed some results obtained for some cases.
...Thank you for posting this paper.
I started going through your equations and found an issue with your definition of the normal vector for the sidewalls.
I believe the correct expression should be
[-x/R * cos(Φ) , -y/R * cos(Φ), sin(Φ)]
This expression is also written in a form that should always be normalized as long as x^2 +y^2 = R^2.
The mistake vanishes when Φ = 0, explaining why you got the expected result for a cylinder. This flows into your other calculations, so I will let you correct this before I review the other technical details more thoroughly.
Actually, I made a mistake while writing the equation on paper, z component of n is not R(z)*sin(Φ), it is R(z)*tan(Φ), which was already correct on the algorithm as you can see on paper. I have uploaded the paper with this correction.
I believe that this is the correct expression
[-x , -y, R(z)tan(Φ)]
Which is further normalized in the algorithm,
I have tried with your expression: [-x/R * cos(Φ) , -y/R * cos(Φ), sin(Φ)], and thrust is still present.
How did you get this expression?
My studies on the EmDrive based on Ray Tracing is done, paper is attached.
In paper it is described how the algorithm was made, and it is discussed some results obtained for some cases.
I'm running some simulations now with higher number of iterations (reflections), but it will take a longer time to get the results. Still with some issues with preallocating memory on the algorithm.
The studies were made considering a continuous beam of photons being reflected inside a truncated cone cavity.
The asymmetry of the cone geometry causes an imbalance in the angle of incidence between the two ends, which I believe is the main cause for the resulting net thust. Calculations with a geometry of a cylinder resulted in zero thrust.
Thrust is towards small end.