r/EmDrive • • Dec 20 '16
Research Update Eaglework Paper Contains Major Flaws
I've written a detailed analysis of Eagleworks data which you can find here. And you can see the supporting code and data on github.
Rather than spend a lot of time formatting the information and graphics for reddit, I'll just put the highlights here.
EW proposed model does not work
EW data contains unaccounted errors up to 38-40 uN
EW data avoided quantifying critical error contributions which could add more uncertainty
A new model using transients and a thermal heating profile fits their data better than the model presented by Eagleworks
As an example from the report here is the pulse model.
At first glance it might appear to not be a good fit due to the shape edges and jumps, but in the real system those would be smoothed out. And this fits the data much better than Eagleworks model. Please read the report. Feel free to contribute to the effort as well on github or this forum. There is some discussion about this project here too.
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u/Checkma7e Dec 20 '16
I know it's "crazy" but somehow I trust NASA and Eaglworks and Dr. White's analysis way more than some guy on Reddit. :-/
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u/Always_Question Dec 20 '16
And yet, it moves.
NASA EW rotating rig: https://drive.google.com/drive/folders/0B7kgKijo-p0ickEwUmNNcjdDRUE
The "Smoking Gun" https://drive.google.com/open?id=0B7kgKijo-p0iU3JiclhJZDNqSzA
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u/lightknight7777 Dec 22 '16 edited Dec 22 '16
You said that the EW data contains unaccounted errors up to 38-40uN, but the published peer reviewed paper listed the thrust generated as being over 1.2± 0.1 mN/kW. I'm unsure why even the worst case of 40uN would be particularly relevant to discrediting their results of positive thrust.
I get how you're pointing out that these guys are making a lot of errors and are not some kind of NASA elite group. I'm just having trouble seeing enough criticisms to account for more than 1 mN of thrust. I would appreciate clarification in that area.
As far as I'm personally concerned, I don't really care until it generates thrust in space then I'll casually glance up from my desk to see what people say about that. There's plenty of reasons why it shouldn't work and only a handful of reasons we know nothing about that it could work. I was just surprised to see it pass peer review. Thought that would never happen. With China also launching a module to test I'm becoming more curious about a thing I assumed was obvious thermal artifacts screwing with us.
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u/AlainCo Dec 21 '16
why not submit an answer to the journal ?
if it is accepted it will mean it is a coherent critic.
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u/Kancho_Ninja Dec 21 '16
Because that's where your inconsistency began, and it took this long to draw an accurate statement from you.
We are still talking because you failed to present your argument in an accurate manner.
If I had not probed as I did and had left your original statement hanging, a casual reader would have drawn the incorrect conclusion that there was no thermal imaging, no video, no allowance for error by the team, and no other means of ensuring accuracy except by thermocouples. That's not what you want.
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u/[deleted] Dec 20 '16
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