After 4 iterations of designing the torsion pendulum I've settled on this aluminum carbon fiber very lightweight platform.
This is a test wire and a little heavier for just testing.
You'll notice the threaded rods on the sides that will be used to beam ballance and the wire goes through the center of a small hole. The wire will be adjusted with weights in the Z and Y dimension on the platform to be in the center of the hole. This assures beam balance.
Underneath the U channel is where the wire is captured 1/2 way between the top and bottom and it's centered to the middle section of the carbon fiber tubes.
The wire tension is set by a guitar Tuner Tuning Peg Machine Head.
This setup even with the heavy wire is extraordinary sensitive and when I finish off the brackets for the frustum and sliding balance weight on the carbon fiber tubes I'll be finishing off the electronics to drive my frustums.
Just a update, back to work.
Shell
battery powered/solar powered portable microwave the size of a thermos bottle.
http://nextbigfuture.com/2016/05/solid-state-rf-technology-enables-cheap.html
This may be of interest to future DIYer EM drive projects
Of particular interest is:
"The technology platform includes NXP’s MKW40Z Kinetis microcontroller (MCU) with a 2.4 GHz signal generator, a MMA25312 pre-driver, MHT1008 driver and MHT1004 final stage amplifier into a single, integrated closed-loop module."
The MKW40Z Kinetis microcontroller comes in a BLE and wireless radio version. If they plan on making this work with your iphone... that would be even better.
Shell,
What hardware are you using to thread the wire through? I don't need to pass through completely like you, but I need something better to grab onto the wire. Please let me know.
I briefly touched on this a few months ago. I'm not in a position where I can experiment right now to verify because I'm in a state of flux of my own. Studying this thing for the past couple of years has me thinking that the resonant rf isn't the cause of the thrust (thousands of times better than a photon rocket), rather it's the perturbation needed. The non Newtonian motion of the matter in the cavity is the final cause. So I propose adding this. A visual:
I never noticed that graphic for Cannae. They use an asymmetric dialectric (cone, pyramid?) inside a symmetric cavity and NASA uses a symmetric dialectric insert in an asymmetric cavity. Those are the inverse of one another geometrically.
Cal Polytech used symmetric insert with symmetric cavity, correct? Did they ever try different shapes of HDPE, like a cone?
I never noticed that graphic for Cannae. They use an asymmetric dialectric (cone, pyramid?) inside a symmetric cavity and NASA uses a symmetric dialectric insert in an asymmetric cavity. Those are the inverse of one another geometrically.
Cal Polytech used symmetric insert with symmetric cavity, correct? Did they ever try different shapes of HDPE, like a cone?
We only had a symmetric cylindrical HDPE disc, but a cone shape was recommended to us by the microwave industry professional who lent us the antenna. He anticipated that a gradually tapered dielectric would mimic a frustum very closely.
Roger Shawyer's first patent has a cone shaped dielectric
I never noticed that graphic for Cannae. They use an asymmetric dialectric (cone, pyramid?) inside a symmetric cavity and NASA uses a symmetric dialectric insert in an asymmetric cavity. Those are the inverse of one another geometrically.
Cal Polytech used symmetric insert with symmetric cavity, correct? Did they ever try different shapes of HDPE, like a cone?
We only had a symmetric cylindrical HDPE disc, but a cone shape was recommended to us by the microwave industry professional who lent us the antenna. He anticipated that a gradually tapered dielectric would mimic a frustum very closely.
Roger Shawyer's first patent has a cone shaped dielectric
I never noticed that graphic for Cannae. They use an asymmetric dialectric (cone, pyramid?) inside a symmetric cavity and NASA uses a symmetric dialectric insert in an asymmetric cavity. Those are the inverse of one another geometrically.
Cal Polytech used symmetric insert with symmetric cavity, correct? Did they ever try different shapes of HDPE, like a cone?
We only had a symmetric cylindrical HDPE disc, but a cone shape was recommended to us by the microwave industry professional who lent us the antenna. He anticipated that a gradually tapered dielectric would mimic a frustum very closely.
Roger Shawyer's first patent has a cone shaped dielectric
I really fail to understand why any serious EmDrive builder is using dielectrics or non freq tunable magnetron based Rf generators with no forward and reflected power feedback?
Roger's best with dielectrics and magnetrons was 16mN at 850W Rf:
http://emdrive.com/feasibilitystudy.html
To get that result his frustum and Rf delivery system build was very complex and featured at least 3 ways to physically tune the frustum and waveguide Rf delivery system.
I measured 8mN at 95W Rf using no dielectric, no physical tuning, no Rf waveguide delivery system and single frequency tunable Rf excitation in TE013 mode with real time forward and reflected power outputs from the 100W Rf amp.
But go your hardest guys, who knows you may get lucky and get a lot of dynamic variables to all hit the force generation sweet spot at the same time.
Because Shawyer used inorganic dielectrics with relative permittivity =38 instead of the materials being discussed.
To understand why anisotropic polymers like PTFE and HDPE, with a relativite permittivity (~2) closer to vacuum and air (~1) than the relative permittivity of the inorganic polymers used by Shawyer (~38) make a difference, one has to have an academic background and engineering experience in Materials Science to tell that what is at stake here is not the dielectric properties but what matters is electrostriction. Also academic background in General Relativity to understand Woodward's Mach effect theory would help in understanding what is at stake.
Because Shawyer used inorganic dielectrics with relative permittivity =38 instead of the materials being discussed.
To understand why anisotropic polymers like PTFE and HDPE, with a relativite permittivity (~2) closer to vacuum and air (~1) than the relative permittivity of the inorganic polymers used by Shawyer (~38) make a difference, one has to have an academic background and engineering experience in Materials Science to tell that what is at stake here is not the dielectric properties but what matters is electrostriction. Also academic background in General Relativity to understand Woodward's Mach effect theory would help in understanding what is at stake.
That is your theory based on no physical experimental data. So why share it to real world EmDrive builders as it may not be correct and may mislead them to obtain null results?
That is your theory based on no physical experimental data. So why share it to real world EmDrive builders as it may not be correct and may mislead them to obtain null results?
Ok, after some reconsideration, I can see how I may be rigorously mistaken in asserting that an EM Drive perhaps is, because of my off-the-cuff fuzzy notions. Rather than thrust (force), lets say transfer efficiency; how much a rocket may increase its velocity for a given amount of energy:
...But, for the interaction with the sun fields, sun plasma, sun photons, a closed and small cavity does not make a big sense. Additionnaly, all the tests were conducted on earth, with earth magnetic field, and not exposed to the interplanetary fields. So, if the emdrive was working with these fields, all the tests that were conducted would be irrelevant. In fact, all the conducted tests are rather supposing a negligeable interaction with external fields. If the aim was of maximizing the interaction with external fields, the device would be completely different.
The idea of the photonic thruster described is that the same photons are used several times, but it works only because there is the mother platform to push against. This is also why the efficiency ratio compared to a photon rocket is decreasing when the speed of the mission spacecraft relatively to the mother platform is increasing.
The energy conservation principle makes that the energy lost by the redshifting photons is gained by the mission spacecraft, in the form of Kinetic Energy relatively to the mother platform. The total momentum of the system composed of the mother platform and the mission spacecraft is not changed. Except when some photons (or waste heat) are lost in space
The emdrive has no mothership to push against, it can not work with the same principle that the Photonic laser thruster

...
1) the electromagnetic pressure is way too small and the GHz frequency too high to envision significant mechanical vibrations of the EM Drive walls. Shawyer claims a maximum of less than 200 milliNewtons, many NASA experiments, particularly in vacuum, and also by Tajmar are in the microNewton range. One can readily show that the mechanical vibrations produced by such forces are of extremely small magnitude. Besides that, the frequency of oscillation of the microwaves is several orders of magnitude higher than typical mechanical vibrations. Therefore the mode shapes would be extremely high and therefore the video is unrepresentative of these extremely tiny vibrations (they would not be flexural vibrations as shown in the video but extremely small motions)


...
1) the electromagnetic pressure is way too small and the GHz frequency too high to envision significant mechanical vibrations of the EM Drive walls. Shawyer claims a maximum of less than 200 milliNewtons, many NASA experiments, particularly in vacuum, and also by Tajmar are in the microNewton range. One can readily show that the mechanical vibrations produced by such forces are of extremely small magnitude. Besides that, the frequency of oscillation of the microwaves is several orders of magnitude higher than typical mechanical vibrations. Therefore the mode shapes would be extremely high and therefore the video is unrepresentative of these extremely tiny vibrations (they would not be flexural vibrations as shown in the video but extremely small motions)
Optical radiation pressure can induce megahertz frequency mechanical oscillations. Or can cool and damp them. See:
http://arxiv.org/abs/1303.0733
The magnetron has a number of resonators. Yang's configuration has a tuned coupling waveguide section. If the frequency seperation of the frustrum and the coupling network and/or magnetron is near a peak on a favorable slope for an acoustic instability, the frustrum (IMHO) just might start singing. But I really doubt it would be for long, considering the disparity of frequencies and sensitivity of the cavity to heat.
Nevertheless, if heat or vibration cause doppler reflected energy that enhances radiation pressure, further heat/pressure will affect the frustrum, and could sustain a resonance.
But the main point is that fundamentally, none of this can result in force/inputPower exceeding the one of a perfectly collimated photon rocket.
But the main point is that fundamentally, none of this can result in force/inputPower exceeding the one of a perfectly collimated photon rocket.
Dr. Rodal, the photonic laser thruster exceeds the force/input power of a photon rocket up to a certain velocity - when the two intersect. If the emrive recycles photons in a similar way, then couldn't it also have a force/input power exceeding a photon rocket up to a certain velocity?
2) how does one recycle photons and exceed a photon rocket force/Input power in a microwave cavity?