Woodward's theory (in his book) on the "propellantless" propulsion claims it needs both simultaneuously the EM flux (delta E) and the changing acceleration of the mass (delta a). In Brito's experiment I see where the Delta E is coming from but what is providing the delta a?
Or was this an unjustified modification to his theory Woodward proposed after Brito's nullification experiment?
<<The observed negative results for [Brito's EM drive] activation in non-modulated power mode, imply that the following theoretical approaches are wholly or partially falsified: Transient mass fluctuation, Thrust predicted according to Woodward’s formulation is around 3.4 mN, thus according to the results reported here no Mach induced mass fluctuation is taking place up to the sensitivity of the experimental apparatus.>>
The theory of the Mach effect thruster (MET) has been written in great detail elsewhere...
[1] H. Fearn & J. F. Woodward, “Recent Results of an Investigation of Mach Effects Thrusters”, Joint Propulsion Conference 2012 to be published in American Institute of Aeronautics and Astronautics.
[2] J. F. Woodward “Making Starships and Stargates” Springer 2013.
Evidently, the simplest Mach effect depends on the square of the acceleration of the body in which it is produced.
To start with, we wish to show that the stack (called N4) is capable of producing a linear thrust. The production of thrust depends on combining a periodic force on an object undergoing periodic mass fluctuations at the frequency of the fluctuations. You also require the appropriate phase so that the force on the object in one part of each cycle is different from that in another part of the cycle.
(We should really multiply by a factor of 4 pi to allow for SI units but as you will see this will still lead to an underestimate.)
Steiner-Martins give 3.2 x10-10 mV-1 for the “d33” piezoelectric constant for the SM-111 material. That is the value of Kp. They list no value for the electrostrictive constant. But electrostrictive effects are generally smaller than piezoelectric effects [3-5]. Using the value for Kp we find
|F|= 191.4 K sub e (12)
(I used the pipe character because of HTML character conflict)
From the power spectrum we can estimate that the electrostrictive constant must be somewhere between 1/6th and 1/10th of the piezoelectric constant. If we take the electrostrictive constant to be 1/8th of the piezoelectric constant, or approximately 4 x 10-11 mV-2, we find that a thrust on the order of 8 nN is predicted. We should in fact multiply by 4π to allow for the SI units, but the observed thrust for these parameters is a couple of microNewtons.
... the condition that the capacitor restmass vary in time is met as the ions in the lattice are accelerated by the changing external electric field.
Some of this energy is likely stored in the gravitational field...
The power amplifier employed was a Carvin DCM 1000 operating in bridged mode.
Take a look at my subsequent comment:
<<But, if electrons are emitted by field emission from a dielectric-resonator experiencing breakdown under the electric field, what happens to the electrons in the air? Is the air also ionized by the electric field? How could that generate propulsion, unless we have a leaky microwave cavity ?>>
These are my malformed , incomplete, thoughts in "poking around" looking for different explanations of the measurements.
If the propulsion is the result of ionized air leaking from the cavity, I see this as much less effective than present ion rockets. Also take into account that they tested thrust pulses for only ~30 sec duration and that would not get us anywhere. A cracked dielectric resonator emitting electrons and/or ionization of air won't work long enough or effectively enough...
Also as far as specific force, the results from the Cannae and Frustum testing were not too encouraging. The Boeing/DARPA specific force tests show an impulse instead of a rectangular pulse. The trips to the moons of Saturn and Jupiter are predicated on very optimistic extrapolations...
Take a look at my subsequent comment:
<<But, if electrons are emitted by field emission from a dielectric-resonator experiencing breakdown under the electric field, what happens to the electrons in the air? Is the air also ionized by the electric field? How could that generate propulsion, unless we have a leaky microwave cavity ?>>
These are my malformed , incomplete, thoughts in "poking around" looking for different explanations of the measurements.
If the propulsion is the result of ionized air leaking from the cavity, I see this as much less effective than present ion rockets. Also take into account that they tested thrust pulses for only ~30 sec duration and that would not get us anywhere. A cracked dielectric resonator emitting electrons and/or ionization of air won't work long enough or effectively enough...
Also as far as specific force, the results from the Cannae and Frustum testing were not too encouraging. The Boeing/DARPA specific force tests show an impulse instead of a rectangular pulse. The trips to the moons of Saturn and Jupiter are predicated on very optimistic extrapolations...
Problem is, I thought that they'd also tested it in a vacume chamber as well and still got positive results.
I may be a bit confused on this one as it seems that I've heard both that they WERE going to test it in a Vacume Chamber and that they HAD tested it in a vacume chamber.
If they haven't yet tested it in a vacume, then your "Ion Wind" theory is possible, but if they have, again, some other mechanism must be at work.
Could someone clear this one up for me, have they or haven't they tested in a vacume chamber and if not, why? It shouldn't be too hard to set up and experiment like this in a vacume chamber. (I do remember some discussion about vacume resistant capacitors, but that should have been corrected by now).
Yes well, you'll have to forgive me that I can't read all what Dr. Rodal is posting. It's pretty obvious he is not familiar with the work. Neither was Brito when he decided to do an M-E experiment using a discarded design a year or two after it had been abandoned.Quote from: Rodal* When did such statements first appear in Woodward's publications?
* What magnitude acceleration is a large “bulk” acceleration according to Woodward?
This is almost asking the right question. It is not the magnitude of the bulk that qualifies it as "bulk" but rather, it is accelerating both ends of the electromechanical spring found in bulk matter. The MLT design used by Brito in the above only accelerated the mobile ion inside the BaTiO3 dielectric cage or lattice. What needs to happen is one accelerates the entire lattice because this includes then, both ends of these EM springs. Accelerating only the mobile ion does not accelerate the entire spring.
Nembo Buldrini's "bulk acceleration conjecture" that corrected the efforts in M-E research was back in early 2008 I believe. It was certainly before Brito's experiments. And again, this is why it is so foolish to do replications or validations of anyone's work without availing oneself to the current state of the art. (And really one hopes people wanting to criticize such work ought to be cognizant of the facts as well.)
I was actually the first to argue that as far as I understood the theory, not just the mobile ion needed to be accelerated, but the entire lattice. Nembo Buldrini then showed this is true from the math and all of the M-E work immediately changed. I was the first to abandon the Mach Lorentz Thruster (the design Brito used) and focus on the previous design, what is now known as the Mach Effect Thruster or MET.
There are two very important aspects to the Bulk Acceleration Conjecture. First is, since the entire active mass material lattice needs to move, it can't be sintered with compounds intended to repress electromechanical responses the way the MLT caps used were, and I presume the caps used by Brito. The lattice needs to accelerate and the magnitude of this acceleration determines both the magnitude of the Mach Effect generated (by the 1w acceleration) and the mass fluctuation rectification into force (by the 2w acceleration). So what it turns out is, the thrust generated from these 1/4 wave oscillator/resonators is quadratic with mechanical Q, and Brito's design had no Q to speak of. It was not a 1/4 wave resonator. If you don't use a reaction mass or acoustic mirror in your design, even given the shabby acceleration generated by ceramics sintered to repress piezo-action and electrostriction, you get 1/2 wave mechanical action which means acceleration in two opposite directions which then cancel each other as regards force generated.
So long story short is, the design used by Brito had been abandoned a year or two before he did his experiment for good reasons and ought not have worked according to theory. This has all been explained by me in several forums over the years, and if Dr. Rodal thinks he is qualified to remark about "moving the goalposts" or whatever, I would just suggest to him he do his homework first. He could for example read Jim's book.
reply from GiThruster regarding Brito's experiments posted by Dr Rodal
...He could for example read Jim's book.

reply from GiThruster regarding Brito's experiments posted by Dr RodalQuote... (0) It's pretty obvious [Rodal] is not familiar with the work.Quote from: Rodal* When did such statements first appear in Woodward's publications?
* What magnitude acceleration is a large “bulk” acceleration according to Woodward?
This is almost asking the right question. It is (1) not the magnitude of the bulk that qualifies it as "bulk" but rather, it is accelerating both ends of the electromechanical spring found in bulk matter. ...
There are two very important aspects to the (2) Bulk Acceleration Conjecture. ...
(3) So long story short is, ... [Rodal] could for example read Jim's book.