Maybe I am misunderstanding but are some of you saying that the limitations on the EW budget may have hampered their paper and the results presented therein?
It certainly has allowed the sceptics to have a field day with it I would say.
With what you did receive it seems that you were able to show over the last 5 years, tests producing tantalizing data. Many here (the press sure knows it) must realize the potential advantage of a propelentless EM engine and have to wonder why it wasn't aggressively pursued with a little more funding and resources.
With a 18.5 billion dollar budget NASA should have earmarked more than they did, NASA surely could afford to do it right and put the question to bed, we all can take advantage of it, if it does.
Shell
While sims like COMSOL and FEKO do show the increasing guide wavelength as the diameter decreases, they don't have the ability, as far as I know, to model the drop in the radiation pressure as the guide wavelength increases.That is entirely backwards. The sims are perfectly capable of providing a way to calculate the forces on each end plate and the sidewalls, and they all will show a larger force on the large plate than the small one, balanced by the force on the sidewalls.
While the distance between the nodes of the standing wave increases towards the small end, "distance between nodes of a standing wave" is not the definition of guide wavelength, and is only meaningful at discrete points, not in the continuously varying way that you use guide wavelength. The models can't provide an answer when you don't have a fully defined question, and you have never properly defined guide wavelength in this context.
Good to know the sims can model the forces. Care to do that and share the data? Plus be sure the equations used to calculated the radiation pressure are compatible with the equations of Cullen.
As the radiation pressure drops much faster than the diameter drop, going from big to small, it is not possible for the sum of all the forces to equal zero.
...
I remember those graphs because the reverse response was so much less than the forward response. If I'm not mistaken that was also when your group started to mitigate the Lorentz error. My conclusion then and now of the reverse graph is that it is due to magnetic interaction. It is the only "thrust" waveform that has the characteristics of a second order step response. There is a fast rise/fall time and an overshoot with ringing. That type of response curve has not been seen again in your results. The second graph is a first order step response; ie:thermal. In a vacuum or low pressure atmosphere the time constant is longer. It would be useful to see a lot more data, even families of plots. For example what would the plots look like if the pressure was stepped down by powers of ten (logrithmically), with everything else the same? My guess is the time constant of the step response would increase as the pressure decreased. Another experiment I have been asking all the em-drive dy people to do is to heat up the Copper cone with resistive heaters and collect data as if it was an RF input. No one has done that yet. I'm sure the EW team has the resources to do this.
The more things you change in an experimental setup the more information you get from your experiments. For example what would happen if the EW team redesigned the mounting hardware that holds the Copper cone on the TP arm. If they could design it so that the CG vs displacement test using the 10 gram weight no longer caused a significant change in displacement how would that affect later tests? It would be interesting to see. I know the EW team has done excellent work and are only interested in finding the truth so I assume they will eventually do some of the things I have suggested.
Zen-in: Please remember that I no longer work at the Eagleworks (EW) Lab and I do not have access to this EW copper frustum test article any longer. I was also working under the direction of Dr. White who did not give me the freedom to pursue a number of tests and thruster optimizations I would have liked to have pursued in the latter part of 2014 till the time I left the EW lab, so a lot of the tests you suggest were thought of, but could not be pursued due to the demands of upper NASA/JSC management. That will change when I get into my new home lab that I will control.
Best, Paul M.
Maybe I am misunderstanding but are some of you saying that the limitations on the EW budget may have hampered their paper and the results presented therein?
It certainly has allowed the sceptics to have a field day with it I would say.
With what you did receive it seems that you were able to show over the last 5 years, tests producing tantalizing data. Many here (the press sure knows it) must realize the potential advantage of a propelentless EM engine and have to wonder why it wasn't aggressively pursued with a little more funding and resources.
With a 18.5 billion dollar budget NASA should have earmarked more than they did, NASA surely could afford to do it right and put the question to bed, we all can take advantage of it, if it does.
Shell
...
HFSS spits out all sorts of computed variables and even allows users to input their own equations using any computed variables. Couldnt power dissipated be computed using surface currents on all walls?
Are there any particular equations that I could try to numerically compute?
Maybe I am misunderstanding but are some of you saying that the limitations on the EW budget may have hampered their paper and the results presented therein?
It certainly has allowed the sceptics to have a field day with it I would say.
With what you did receive it seems that you were able to show over the last 5 years, tests producing tantalizing data. Many here (the press sure knows it) must realize the potential advantage of a propelentless EM engine and have to wonder why it wasn't aggressively pursued with a little more funding and resources.
With a 18.5 billion dollar budget NASA should have earmarked more than they did, NASA surely could afford to do it right and put the question to bed, we all can take advantage of it, if it does.
Shell
Shell:
From its inception, the EW lab's yearly budget was on a shoe-string and it never exceeded $50k per year for build-material and new test equipment with everything else being bootlegged from NASA surplus storage at JSC after the end of the Space Shuttle program. The civil-servant outfit Dr. White works for, NASA/JSC/EP4 used free-to-them JSC division's civil-servant's part-time labor when needed, or civil-servant/college sponsored student co-op help during the first ~3 years of the lab's existence to help with the EW lab buildup and calibration. They re-hired me in May 2011 from a layoff status that started back in December 2010 when I got laid off from the Orion project, as only a part-time, temporary employee with NO benefits with just enough $$ in the EW pot to cover my base NASA 40 hr/wk contractor salary for the first three years, and then less as my time was scaled back down to ~24 hours per week max for the last ~18 months I worked at the EW. And I was also expected to buy small parts out of my own cash reserves as well, so you do the math. It appears that most managers at JSC wanted what the EM-drive thruster technology could provide them, but none of them wanted to be the ones paying for its development. However and more importantly, other than Dr. White, they didn't want to risk their reputations if it didn't work.
Best, Paul M.
but none of them wanted to be the ones paying for its development. However and more importantly, other than Dr. White, they didn't want to risk their reputations if it didn't work.
Maybe I am misunderstanding but are some of you saying that the limitations on the EW budget may have hampered their paper and the results presented therein?
It certainly has allowed the sceptics to have a field day with it I would say.
With what you did receive it seems that you were able to show over the last 5 years, tests producing tantalizing data. Many here (the press sure knows it) must realize the potential advantage of a propelentless EM engine and have to wonder why it wasn't aggressively pursued with a little more funding and resources.
With a 18.5 billion dollar budget NASA should have earmarked more than they did, NASA surely could afford to do it right and put the question to bed, we all can take advantage of it, if it does.
Shell
Shell:
From its inception, the EW lab's yearly budget was on a shoe-string and it never exceeded $50k per year for build-material and new test equipment with everything else being bootlegged from NASA surplus storage at JSC after the end of the Space Shuttle program. The civil-servant outfit Dr. White works for, NASA/JSC/EP4 used free-to-them JSC division's civil-servant's part-time labor when needed, or civil-servant/college sponsored student co-op help during the first ~3 years of the lab's existence to help with the EW lab buildup and calibration. They re-hired me in May 2011 from a layoff status that started back in December 2010 when I got laid off from the Orion project, as only a part-time, temporary employee with NO benefits with just enough $$ in the EW pot to cover my base NASA 40 hr/wk contractor salary for the first three years, and then less as my time was scaled back down to ~24 hours per week max for the last ~18 months I worked at the EW. And I was also expected to buy small parts out of my own cash reserves as well, so you do the math. It appears that most managers at JSC wanted what the EM-drive thruster technology could provide them, but none of them wanted to be the ones paying for its development. However and more importantly, other than Dr. White, they didn't want to risk their reputations if it didn't work.
Best, Paul M.Quotebut none of them wanted to be the ones paying for its development. However and more importantly, other than Dr. White, they didn't want to risk their reputations if it didn't work.
Geez, don't they realize that it could be a win-win decision. Looking at their perspective... If it doesn't work you have debunked years of hype that it does, you win. If it works it's a bigger win.
Shell
...
Shell:
From its inception, the EW lab's yearly budget was on a shoe-string and it never exceeded $50k per year for build-material and new test equipment with everything else being bootlegged from NASA surplus storage at JSC after the end of the Space Shuttle program. The civil-servant outfit Dr. White works for, NASA/JSC/EP4 used free-to-them JSC division's civil-servant's part-time labor when needed, or civil-servant/college sponsored student co-op help during the first ~3 years of the lab's existence to help with the EW lab buildup and calibration. They re-hired me in May 2011 from a layoff status that started back in December 2010 when I got laid off from the Orion project, as only a part-time, temporary employee with NO benefits with just enough $$ in the EW pot to cover my base NASA 40 hr/wk contractor salary for the first three years, and then less as my time was scaled back down to ~24 hours per week max for the last ~18 months I worked at the EW. And I was also expected to buy small parts out of my own cash reserves as well, so you do the math. It appears that most managers at JSC wanted what the EM-drive thruster technology could provide them, but none of them wanted to be the ones paying for its development. However and more importantly, other than Dr. White, they didn't want to risk their reputations if it didn't work.
Best, Paul M.
)...
HFSS spits out all sorts of computed variables and even allows users to input their own equations using any computed variables. Couldnt power dissipated be computed using surface currents on all walls?
Are there any particular equations that I could try to numerically compute?HFSS is owned by ANSYS (overall, a more powerful program than COMSOL or FEKO). Do you call it HFSS because you have a version prior to the acquisition by ANSYS or because you are only running the HFSS module?
COMSOL also allows the user to write equations, and so do other programs like ABAQUS, etc.
The problem with using codes like this to calculate a new theory are multifold:
1) These packages are black boxes, and the user does not have complete knowledge of the actual solution algorithms being employed.
2) For a new theory like Todd's one may be unable to actually code a solution because certain variables in the theory are not being computed by the program. For example I am still surprised that none of the solutions posted by Monomorphic show the quality factor of resonance Q. Can FEKO calculate the Q? (COMSOL can). But the Q is easy to calculate compared with other variables that one may need to calculate in a new theory (for example one may need to calculate spatial derivatives of certain functions and these numerical methods are particularly bad concerning accuracy of derivatives. One may need to satisfy higher order boundary conditions, etc.).
"...From its inception, the EW lab's yearly budget was on a shoe-string and it never exceeded $50k per year for build-material and new test equipment with everything else being bootlegged from NASA surplus storage at JSC after the end of the Space Shuttle program...."
but none of them wanted to be the ones paying for its development. However and more importantly, other than Dr. White, they didn't want to risk their reputations if it didn't work.
Geez, don't they realize that it could be a win-win decision. Looking at their perspective... If it doesn't work you have debunked years of hype that it does, you win. If it works it's a bigger win.
Maybe I am misunderstanding but are some of you saying that the limitations on the EW budget may have hampered their paper and the results presented therein?
It certainly has allowed the sceptics to have a field day with it I would say.
With what you did receive it seems that you were able to show over the last 5 years, tests producing tantalizing data. Many here (the press sure knows it) must realize the potential advantage of a propelentless EM engine and have to wonder why it wasn't aggressively pursued with a little more funding and resources.
With a 18.5 billion dollar budget NASA should have earmarked more than they did, NASA surely could afford to do it right and put the question to bed, we all can take advantage of it, if it does.
Shell
Shell:
From its inception, the EW lab's yearly budget was on a shoe-string and it never exceeded $50k per year for build-material and new test equipment with everything else being bootlegged from NASA surplus storage at JSC after the end of the Space Shuttle program. The civil-servant outfit Dr. White works for, NASA/JSC/EP4 used free-to-them JSC division's civil-servant's part-time labor when needed, or civil-servant/college sponsored student co-op help during the first ~3 years of the lab's existence to help with the EW lab buildup and calibration. They re-hired me in May 2011 from a layoff status that started back in December 2010 when I got laid off from the Orion project, as only a part-time, temporary employee with NO benefits with just enough $$ in the EW pot to cover my base NASA 40 hr/wk contractor salary for the first three years, and then less as my time was scaled back down to ~24 hours per week max for the last ~18 months I worked at the EW. And I was also expected to buy small parts out of my own cash reserves as well, so you do the math. It appears that most managers at JSC wanted what the EM-drive thruster technology could provide them, but none of them wanted to be the ones paying for its development. However and more importantly, other than Dr. White, they didn't want to risk their reputations if it didn't work.
Best, Paul M.Quotebut none of them wanted to be the ones paying for its development. However and more importantly, other than Dr. White, they didn't want to risk their reputations if it didn't work.
Geez, don't they realize that it could be a win-win decision. Looking at their perspective... If it doesn't work you have debunked years of hype that it does, you win. If it works it's a bigger win.
Shell
"...From its inception, the EW lab's yearly budget was on a shoe-string and it never exceeded $50k per year for build-material and new test equipment with everything else being bootlegged from NASA surplus storage at JSC after the end of the Space Shuttle program...."Quite frankly, I'm stunned. $50K out of a budget as big as they have? It feels like they were more interested in being able to say they "have" an advanced research group, then actually doing research.
"...From its inception, the EW lab's yearly budget was on a shoe-string and it never exceeded $50k per year for build-material and new test equipment with everything else being bootlegged from NASA surplus storage at JSC after the end of the Space Shuttle program...."Quite frankly, I'm stunned. $50K out of a budget as big as they have? It feels like they were more interested in being able to say they "have" an advanced research group, then actually doing research.
What Eagle Works is doing is really experimental physics. That is way outside the charter of JSC. Heck, it's even way outside the charter of NASA. JSC is really supposed to be more oriented toward operational aspects of NASA's programs. Ames and Langley are the more research-oriented NASA centers. So, it's not really a surprise that JSC can really only find small amounts of money for a group doing basic experimental physics. None of the money provided to JSC is actually really meant for an experimental physics program.
When the US government wants to spend money on experimental physics, that money normally goes to the Department of Energy, DARPA, the National Science Foundation, etc. -- agencies that are set up to fund basic science research.
"...From its inception, the EW lab's yearly budget was on a shoe-string and it never exceeded $50k per year for build-material and new test equipment with everything else being bootlegged from NASA surplus storage at JSC after the end of the Space Shuttle program...."Quite frankly, I'm stunned. $50K out of a budget as big as they have? It feels like they were more interested in being able to say they "have" an advanced research group, then actually doing research.
What Eagle Works is doing is really experimental physics. That is way outside the charter of JSC. Heck, it's even way outside the charter of NASA. JSC is really supposed to be more oriented toward operational aspects of NASA's programs. Ames and Langley are the more research-oriented NASA centers. So, it's not really a surprise that JSC can really only find small amounts of money for a group doing basic experimental physics. None of the money provided to JSC is actually really meant for an experimental physics program.
When the US government wants to spend money on experimental physics, that money normally goes to the Department of Energy, DARPA, the National Science Foundation, etc. -- agencies that are set up to fund basic science research.
If we are going to talk about pure utility the argument could be made that throwing vast amounts of taxpayer money down the black hole that is the National Ignition Facility, something that is probably never going to produce a useful form of Nuclear Fusion isn't the best of investments.
...
Shell:
From its inception, the EW lab's yearly budget was on a shoe-string and it never exceeded $50k per year for build-material and new test equipment with everything else being bootlegged from NASA surplus storage at JSC after the end of the Space Shuttle program. The civil-servant outfit Dr. White works for, NASA/JSC/EP4 used free-to-them JSC division's civil-servant's part-time labor when needed, or civil-servant/college sponsored student co-op help during the first ~3 years of the lab's existence to help with the EW lab buildup and calibration. They re-hired me in May 2011 from a layoff status that started back in December 2010 when I got laid off from the Orion project, as only a part-time, temporary employee with NO benefits with just enough $$ in the EW pot to cover my base NASA 40 hr/wk contractor salary for the first three years, and then less as my time was scaled back down to ~24 hours per week max for the last ~18 months I worked at the EW. And I was also expected to buy small parts out of my own cash reserves as well, so you do the math. It appears that most managers at JSC wanted what the EM-drive thruster technology could provide them, but none of them wanted to be the ones paying for its development. However and more importantly, other than Dr. White, they didn't want to risk their reputations if it didn't work.
Best, Paul M.
It is good to know the real situation, as it shows the truth. Contrast this with articles about the EM Drive being tested in the X-37B without any evidence or justification (why use something as valuable as the X-37B which has other purposes)
http://www.ibtimes.co.uk/space-race-revealed-us-china-test-futuristic-emdrive-tiangong-2-mysterious-x-37b-plane-1590289
and people that post about Boeing going "dark" with the Shawyer project, when the evidence (and the people at Boeing) points otherwise, as to what really happened.
Wonder whether Cannae will really test theirs into Space (hopefully soon), and whether they will make the information available real time...
http://cannae.com/cannae-is-developing-a-cubesat-thruster/
. The Vulcans arrive 15 minutes after the Cannae cube-sat is activated.
...snip...
The doorway to a levitator is again open.
YES I will finish the rotary test rig program and release the data as I consider it vital to have data showing Q dropping or not as acceleration occurs and to plot the cavity energy & momentum loss or not against test rig gained angular KE as velocity increases vs power supply energy supply rate change or not.
Phil
Thus all could change with a new administration coming in. Reports are circulating that Leo and earth science should take a back seat to space exploration.
https://www.yahoo.com/news/trump-administration-set-eliminate-nasa-035716399.html
List of unaddressed or missing issues from the recent EW paper via a poster on Reddit.
https://drive.google.com/file/d/0B6juR48k_XoTREUxc1QycWxwZ2M/view
See what you think?
"...From its inception, the EW lab's yearly budget was on a shoe-string and it never exceeded $50k per year for build-material and new test equipment with everything else being bootlegged from NASA surplus storage at JSC after the end of the Space Shuttle program...."Quite frankly, I'm stunned. $50K out of a budget as big as they have? It feels like they were more interested in being able to say they "have" an advanced research group, then actually doing research.
What Eagle Works is doing is really experimental physics. That is way outside the charter of JSC. Heck, it's even way outside the charter of NASA. JSC is really supposed to be more oriented toward operational aspects of NASA's programs. Ames and Langley are the more research-oriented NASA centers. So, it's not really a surprise that JSC can really only find small amounts of money for a group doing basic experimental physics. None of the money provided to JSC is actually really meant for an experimental physics program.
When the US government wants to spend money on experimental physics, that money normally goes to the Department of Energy, DARPA, the National Science Foundation, etc. -- agencies that are set up to fund basic science research.