It would appear from the comments made here, the full EW paper has reached beyond EWs and AIAA. Seems Dr White sent it to Mark Rademaker, who modelled Dr White's IXS Enterprise warp ship. I predict it will see the light of day well before AIAA publishes it.
http://www.forbes.com/sites/startswithabang/2016/09/02/nasas-impossible-space-engine-the-emdrive-passes-peer-review/#6ab6875a692c
The information below was not in that released by Dr. Rodal. It must be from the full paper:QuoteFor the EMdrive, the device that was tested here, thrust was consistently observed on the device to be between 30-and-50 microNewtons, giving us that 1.2 N/MW figure. But the limits of the measuring device’s threshold was just 10-to-15 microNewtons! In other words, these results may be consistent and interesting, but this isn’t as robust as anyone wants it to be.
I am disappointed to see that "30-50 microNewtons" number. It is just in the range of Lorentz force you would see with a few amperes DC, several hundred cm^2 closed current loop, and the earth's magnet field. It looks like they did not avoid the same old flaw they made in their 2014 paper (see http://arxiv.org/pdf/1510.07752v1 for that flaw). After all, they got to know that flaw after their new test was done.
It would appear from the comments made here, the full EW paper has reached beyond EWs and AIAA. Seems Dr White sent it to Mark Rademaker, who modelled Dr White's IXS Enterprise warp ship. I predict it will see the light of day well before AIAA publishes it.
http://www.forbes.com/sites/startswithabang/2016/09/02/nasas-impossible-space-engine-the-emdrive-passes-peer-review/#6ab6875a692c
The information below was not in that released by Dr. Rodal. It must be from the full paper:
...
It would appear from the comments made here, the full EW paper has reached beyond EWs and AIAA. Seems Dr White sent it to Mark Rademaker, who modelled Dr White's IXS Enterprise warp ship. I predict it will see the light of day well before AIAA publishes it.
http://www.forbes.com/sites/startswithabang/2016/09/02/nasas-impossible-space-engine-the-emdrive-passes-peer-review/#6ab6875a692c
The information below was not in that released by Dr. Rodal. It must be from the full paper:
...
What is your evidence that it "must" be from the full paper? Have you seen the full paper?
I would suggest you refrain from absolute statements like this until you have.
Thought provoking: the results reported (if true) in the up coming peer reviewed paper from EWL indicates 1.2 mN/kilowatt in TM212, when their first campaign indicated a far great force/kilowatt 21.3 mN/kW in TE012....No small difference! Sonny stated that they couldn't get any more than 2.6 Watts into their frustum at that time in that particular configuration.
One would expect that EWL would design a "better" antenna (hoop vs. loop) and place it in a "better" location in order to put more energy into this higher force producing mode.
Not to forget that EWL also intended to employ PPL expressly to test several different modes and frequencies that might lie "close" to one another. While EWL was able to get more power and a higher overall force measurement in TM212, the fact remains that TE012 produced a much great force/Watt measurement. Indeed we'll have to wait for the paper, but if it has been leaked, I hope it comes our way, and soon! Image attached: TE012 satellite station keeping sized (10 cm base Diam.) thruster. (2.1mN/100W w/out spherical caps.)
. Going to PM to "spreche mit X_Ray jetzt" Ciao PS: attached is sim of NASA's frustum TE012 at 1.8804 GHz..2.6 Watts.
I am disappointed to see that "30-50 microNewtons" number. It is just in the range of Lorentz force you would see with a few amperes DC, several hundred cm^2 closed current loop, and the earth's magnet field. It looks like they did not avoid the same old flaw they made in their 2014 paper (see http://arxiv.org/pdf/1510.07752v1 for that flaw). After all, they got to know that flaw after their new test was done.
.../...
I am disappointed to see that "30-50 microNewtons" number. It is just in the range of Lorentz force you would see with a few amperes DC, several hundred cm^2 closed current loop, and the earth's magnet field. It looks like they did not avoid the same old flaw they made in their 2014 paper (see http://arxiv.org/pdf/1510.07752v1 for that flaw). After all, they got to know that flaw after their new test was done.
As I recall, their final apparatus was using a solid state RF source so the Lorenz force may have been less that what you refer to. Both EW and Tajmar had to use fairly small vacuum chambers so they were restricted as to the type and size of RF sources, cavities, etc. One of the great hopes for the EW paper was that one of the other NASA labs would take pity on them and loan them a larger chamber for a bigger rig that could provide more definitive thrust levels.
The bane of EM Drive Science - minuscule vacuum chambers.
Their 2014 paper used solid state RF source too. They got to know that flaw from my paper after their new test was done, but now it seems likely they did not redo the tests.
It would appear from the comments made here, the full EW paper has reached beyond EWs and AIAA. Seems Dr White sent it to Mark Rademaker, who modelled Dr White's IXS Enterprise warp ship. I predict it will see the light of day well before AIAA publishes it.
http://www.forbes.com/sites/startswithabang/2016/09/02/nasas-impossible-space-engine-the-emdrive-passes-peer-review/#6ab6875a692c
The information below was not in that released by Dr. Rodal. It must be from the full paper:
...
What is your evidence that it "must" be from the full paper? Have you seen the full paper?
I would suggest you refrain from absolute statements like this until you have.
There are data stated in the Forbes article that are not in the data Dr. Rodal shared. That is clear.
So either the Forbes article writer made them up or he read them from the report. Which seems most likely, the writer made them up and created a time bomb for himself or he quoted from the paper?
http://www.forbes.com/sites/startswithabang/2016/09/02/nasas-impossible-space-engine-the-emdrive-passes-peer-review/#6ab6875a692c
Curious article this as it seems to be just going round the same course as previously. I thought one of the things Eagleworks were doing was looking for an 'exhaust' in fact that was the whole point of their theory of explanation.
http://www.forbes.com/sites/startswithabang/2016/09/02/nasas-impossible-space-engine-the-emdrive-passes-peer-review/#6ab6875a692c
Curious article this as it seems to be just going round the same course as previously. I thought one of the things Eagleworks were doing was looking for an 'exhaust' in fact that was the whole point of their theory of explanation.
About this matter, please see my exchange with Ethan on twitter https://twitter.com/StartsWithABang/status/771710336248389633. I pointed out to him a couple of things he was not aware of.
Also in spite of what some articles are saying the EM drive if it works doesn't really tip up the whole basis of modern physics into the air, as the only place it does impact current physics is how we think of and define the QV?
...
Thanks for the link.
Also in spite of what some articles are saying the EM drive if it works doesn't really tip up the whole basis of modern physics into the air, as the only place it does impact current physics is how we think of and define the QV?
Also in spite of what some articles are saying the EM drive if it works doesn't really tip up the whole basis of modern physics into the air, as the only place it does impact current physics is how we think of and define the QV?
If the EM drive works, assuming thrust can be shown to be beyond any experimental error, that doesn't mean all of physics is wrong. It just means we don't know how the EM drive works. Maybe it interacts with the QV, gravitational field, Mach Effect, Roger is right, etc.
We'll have to wait for the paper to see if there are experimental errors that could account for the thrust. Thermal, magnetic, and outgassing are possibilities. Testing in vacuum should help with thermal issues.
If there is beyond any doubt anomalous thrust, that should keep the theorists busy for quite some time.
The information that I relayed to X_Ray came from the "Emdrive Experimental Results" page...apparently this is TE211 and not TM212.
"TM212 [13] Ambient 0.2286 0.2794 0.15875 0.3111 0.5475 14.78 extruded HDPE relative permitt. =2.26@1-3GHz 1.9367 16.7 18100 0.0501 3.00 899"
There is apparent confusion here (most likely on my part), but am continuing to study this. Any input would be appreciated. Thnx , FL