I can do a time domain analysis, but that requires quite a bit of computation. Due to the complex geometry of the cannae drive, it has quite a few triangles in the 3d mesh - which also adds dramatically to compute time.
Dr. Rodal, Todd, Paul March, Dr. Woodward, Dr. Hiedi Fern, Dr. Martin Tajmar along with many other other physicists, engineers and experts in propulsion.
2 : Emdrive works, and does not violate CoE, because it exists non classical reference frames to define appropriately Kinetic Energy, and the Emdrive does not give a constant acceleration, but an acceleration decreasing proportionnaly to the speed. New physics needed.
How can acceleration be decreasing proportional to the speed? This would mean that acceleration would be measured differently in different frames of reference (i.e. it would have to be higher in a frame co-moving with the rocket w/o acceleration). How is that possible?
Dr. Rodal, Todd, Paul March, Dr. Woodward, Dr. Hiedi Fern, Dr. Martin Tajmar along with many other other physicists, engineers and experts in propulsion.
Ahhhhh... To have been a fly on the wall during those discussion sessions!
You have to love the internet and thank SSi.org taking the time to make this breakthrough propulsion workshop available to the world.
Is Professor Woodward on the photo ?
Shawyer's description of how the device works (which is what started this conversation) does not have it pushing on anything, so according to Shawyer's claims it would be a free energy device.
His claim is a small % of the momentum in the internal EmWave is transferred to the external frustum. Most of the energy in the frustum exits as heat as in the attached image from his peer reviewed paper.
Bottom line is the EmDrive generates a force and accelerates a mass while it consumes energy to do so.
What referential for Kinetic Energy ? in GR you do not have an absolute reference frame. What is your reference frame for Kinetic Energy ?
As I calculated a few pages ago, the 0.67C (relatively to the earth referential) mentionned in the Shawyer peer-rewieved paper means a Kinetic Energy of 3.1191599*10^20 joules
Since the 10 years of operation of the 200Kwe generator gives only 6.311*10^13 Joules
So, following Shawyer, at the expanse of 6.311*10^13 Joules a spaceship can get 3.1191599* 10^20 joules of Kinetic Energy. We get massive free energy !
No, you don't get massive 'free' energy. What you get is different energies in different reference frames. You can see that simply by the following example. Say a ship is moving wrt earth frame at just under 0.5c by 1000m/s and you observe it. The ship makes a burn to increase its velocity wrt you by 1000m/s to exactly 0.5c wrt you. For a 10,000kg ship, how much energy does the pilot need to add? It depends on which reference frame. In the ships frame the pilot only needs to do the same burn to gain 1000m/s as always which is 5E9 J. You would say its about 1.5E15 J. It does gain that but not by the ship expending that energy in its reference frame. It would be the same regardless of a rocket of an EmDrive engine except the EmDrive would be more efficient. No doubt some will claim the rocket fuel already has kinetic energy, which it does, but that's natures gift, not something the ship had to provide by internal energy release stored as fuel because it never had that energy content to begin with. If someone objects further then consider that the ship was launched from a planet already moving at just under 05c to start with.
The bottom line is that the actual energy to get to the stars is probably a lot less that convention dictates.
P.S. I understand Woodward and allies previously released an essay demolishing the free energy or over unity arguments.
http://ssi.org/epi/Over-Unity_Argument_&_Mach_Effect_Thrusters.pdf
Was that discussed at the workshop?
Shawyer's description of how the device works (which is what started this conversation) does not have it pushing on anything, so according to Shawyer's claims it would be a free energy device.
His claim is a small % of the momentum in the internal EmWave is transferred to the external frustum. Most of the energy in the frustum exits as heat as in the attached image from his peer reviewed paper.
Bottom line is the EmDrive generates a force and accelerates a mass while it consumes energy to do so.
What referential for Kinetic Energy ? in GR you do not have an absolute reference frame. What is your reference frame for Kinetic Energy ?
As I calculated a few pages ago, the 0.67C (relatively to the earth referential) mentionned in the Shawyer peer-rewieved paper means a Kinetic Energy of 3.1191599*10^20 joules
Since the 10 years of operation of the 200Kwe generator gives only 6.311*10^13 Joules
So, following Shawyer, at the expanse of 6.311*10^13 Joules a spaceship can get 3.1191599* 10^20 joules of Kinetic Energy. We get massive free energy !
No, you don't get massive 'free' energy. What you get is different energies in different reference frames. You can see that simply by the following example. Say a ship is moving wrt earth frame at just under 0.5c by 1000m/s and you observe it. The ship makes a burn to increase its velocity wrt you by 1000m/s to exactly 0.5c wrt you. For a 10,000kg ship, how much energy does the pilot need to add? It depends on which reference frame. In the ships frame the pilot only needs to do the same burn to gain 1000m/s as always which is 5E9 J. You would say its about 1.5E15 J. It does gain that but not by the ship expending that energy in its reference frame. It would be the same regardless of a rocket of an EmDrive engine except the EmDrive would be more efficient. No doubt some will claim the rocket fuel already has kinetic energy, which it does, but that's natures gift, not something the ship had to provide by internal energy release stored as fuel because it never had that energy content to begin with. If someone objects further then consider that the ship was launched from a planet already moving at just under 05c to start with.
The bottom line is that the actual energy to get to the stars is probably a lot less that convention dictates.
P.S. I understand Woodward and allies previously released an essay demolishing the free energy or over unity arguments.
http://ssi.org/epi/Over-Unity_Argument_&_Mach_Effect_Thrusters.pdf
Was that discussed at the workshop?
We routinely hear a criticism of METs based upon an argument that claims: if a
MET is operated at constant power input for a sufficiently long time, it will acquire
enough kinetic energy to exceed the total input energy of operation. Assuming this
argument to be correct, critcs assert that METs violate energy conservation as the ratio of
the acquired kinetic energy to total input energy exceeds “unity.”
Contrary to this “over-unity” assumption, this argument is based on flawed
physics and, consequently, wrong. The fact that the argument applies to all simple
mechanical systems (in addition to METs) should have alerted critics to their mistake.
But it didn’t.
So, a dumb idea that should have been quickly buried is still with us. The
purpose of this essay is to carry out a long overdue burial.
No, you don't get massive 'free' energy. What you get is different energies in different reference frames. You can see that simply by the following example. Say a ship is moving wrt earth frame at just under 0.5c by 1000m/s and you observe it. The ship makes a burn to increase its velocity wrt you by 1000m/s to exactly 0.5c wrt you. For a 10,000kg ship, how much energy does the pilot need to add? It depends on which reference frame. In the ships frame the pilot only needs to do the same burn to gain 1000m/s as always which is 5E9 J. You would say its about 1.5E15 J. It does gain that but not by the ship expending that energy in its reference frame. It would be the same regardless of a rocket of an EmDrive engine except the EmDrive would be more efficient. No doubt some will claim the rocket fuel already has kinetic energy, which it does, but that's natures gift, not something the ship had to provide by internal energy release stored as fuel because it never had that energy content to begin with. If someone objects further then consider that the ship was launched from a planet already moving at just under 05c to start with.
The bottom line is that the actual energy to get to the stars is probably a lot less that convention dictates.
P.S. I understand Woodward and allies previously released an essay demolishing the free energy or over unity arguments.
http://ssi.org/epi/Over-Unity_Argument_&_Mach_Effect_Thrusters.pdf
Was that discussed at the workshop?
Correct.
In the ship's frame, the only one which matters, the energy needed to alter velocity in relation to some desired destination is always the same as the ship's mass does not alter. Well not so much as it matters.
BTW Jim Woodward makes a good comment:
http://ssi.org/epi/Over-Unity_Argument_&_Mach_Effect_Thrusters.pdfQuoteWe routinely hear a criticism of METs based upon an argument that claims: if a
MET is operated at constant power input for a sufficiently long time, it will acquire
enough kinetic energy to exceed the total input energy of operation. Assuming this
argument to be correct, critcs assert that METs violate energy conservation as the ratio of
the acquired kinetic energy to total input energy exceeds “unity.”
Contrary to this “over-unity” assumption, this argument is based on flawed
physics and, consequently, wrong. The fact that the argument applies to all simple
mechanical systems (in addition to METs) should have alerted critics to their mistake.
But it didn’t.
So, a dumb idea that should have been quickly buried is still with us. The
purpose of this essay is to carry out a long overdue burial.
Interesting paper. I glanced at it and found the math was within my ability. So I printed it out to take a closer look. I think I will be able to find something wrong in his argument. But I may not be able to. Whatever the result is, I will write a swift report about my findings.
Interesting paper. I glanced at it and found the math was within my ability. So I printed it out to take a closer look. I think I will be able to find something wrong in his argument. But I may not be able to. Whatever the result is, I will write a swift report about my findings.
This thread might help you find out what's wrong with his arguments... https://forum.nasaspaceflight.com/index.php?topic=31037.0
There is no single frame of reference "that matters". All frames of reference matter.
Interesting paper. I glanced at it and found the math was within my ability. So I printed it out to take a closer look. I think I will be able to find something wrong in his argument. But I may not be able to. Whatever the result is, I will write a swift report about my findings.
This thread might help you find out what's wrong with his arguments... https://forum.nasaspaceflight.com/index.php?topic=31037.0
There is no single frame of reference "that matters". All frames of reference matter.
Only the ship's frame matters as it alters ship's velocity, relative to a desired destination, with a constant relationship between work done on the ship's mass and velocity.
To the ship, accelerating at a constant rate, there is no velocity, just acceleration.
Interesting paper. I glanced at it and found the math was within my ability. So I printed it out to take a closer look. I think I will be able to find something wrong in his argument. But I may not be able to. Whatever the result is, I will write a swift report about my findings.
This thread might help you find out what's wrong with his arguments... https://forum.nasaspaceflight.com/index.php?topic=31037.0
There is no single frame of reference "that matters". All frames of reference matter.
Only the ship's frame matters as it alters ship's velocity, relative to a desired destination, with a constant relationship between work done on the ship's mass and velocity.
To the ship, accelerating at a constant rate, there is no velocity, just acceleration.
Earth frame matters too. Because if a ship, after a dozen or so years of acceleration, hits the Earth,the Earth will break into a pile of asteroids. But I think there still can be math errors with the ship frame. Let me see whether I can be lucky.
...
In the ship's frame, the only one which matters, the energy needed to alter velocity in relation to some desired destination is always the same as the ship's mass does not alter. Well not so much as it matters.
BTW Jim Woodward makes a good comment:
http://ssi.org/epi/Over-Unity_Argument_&_Mach_Effect_Thrusters.pdfQuoteWe routinely hear a criticism of METs based upon an argument that claims: if a
MET is operated at constant power input for a sufficiently long time, it will acquire
enough kinetic energy to exceed the total input energy of operation. Assuming this
argument to be correct, critcs assert that METs violate energy conservation as the ratio of
the acquired kinetic energy to total input energy exceeds “unity.”
Contrary to this “over-unity” assumption, this argument is based on flawed
physics and, consequently, wrong. The fact that the argument applies to all simple
mechanical systems (in addition to METs) should have alerted critics to their mistake.
But it didn’t.
So, a dumb idea that should have been quickly buried is still with us. The
purpose of this essay is to carry out a long overdue burial.
Now we have done something stupid and wrong.
But this is the mathematics of those who make the “over unity” energy conservation violation argument about the operation of METs. The real question here is how could anyone, having done this
calculation or its equivalent, think that they had made a profound discovery about anything?
We know that, starting from t= 0, if we let the integration interval t get very large, the work equation integral will first equal and then exceed the energy calculated by the figure of merit equation. So we require that t be sufficiently small that this obvious violation of energy conservation does not happen.
....
All inertial (constant velocity) frames matter, because physics is the same in all inertial frames. This is the fundamental principle of relativity. If you want to jump between frames, then you have to start being careful with transformations, and generally you can't compare energy between frames. Conservation of energy as normally discussed requires you to be talking about a single inertial reference frame. Being in the accelerating frame of the ship requires you to account for non-inertial effects, just like how the Coriolis effect appears if you are in a rotating frame.
Interesting paper. I glanced at it and found the math was within my ability. So I printed it out to take a closer look. I think I will be able to find something wrong in his argument. But I may not be able to. Whatever the result is, I will write a swift report about my findings.
This thread might help you find out what's wrong with his arguments... https://forum.nasaspaceflight.com/index.php?topic=31037.0
There is no single frame of reference "that matters". All frames of reference matter.
Only the ship's frame matters as it alters ship's velocity, relative to a desired destination, with a constant relationship between work done on the ship's mass and velocity.
To the ship, accelerating at a constant rate, there is no velocity, just acceleration.
Earth frame matters too. Because if a ship, after a dozen or so years of acceleration, hits the Earth,the Earth will break into a pile of asteroids. But I think there still can be math errors with the ship frame. Let me see whether I can be lucky.
The Earth's frame only matters if an inbound ship needs to match velocity.
However the work needed to be done on the ship's mass to alter the relative velocity to 0, in the ship's frame, stays constant and that is the only effect that is important.
All inertial (constant velocity) frames matter, because physics is the same in all inertial frames. This is the fundamental principle of relativity.

2 : Emdrive works, and does not violate CoE, because it exists non classical reference frames to define appropriately Kinetic Energy, and the Emdrive does not give a constant acceleration, but an acceleration decreasing proportionnaly to the speed. New physics needed.
How can acceleration be decreasing proportional to the speed? This would mean that acceleration would be measured differently in different frames of reference (i.e. it would have to be higher in a frame co-moving with the rocket w/o acceleration). How is that possible?
The work done by a constant force of magnitude F on a point that moves a displacement (not distance) s in the direction of the force is the product
W = F s {\displaystyle W=Fs} {\displaystyle W=Fs}.
For example, if a force of 10 newtons (F = 10 N) acts along a point that travels 2 metres (s = 2 m), then it does the work W = (10 N)(2 m) = 20 N m = 20 J. This is approximately the work done lifting a 1 kg weight from ground to over a person's head against the force of gravity. Notice that the work is doubled either by lifting twice the weight the same distance or by lifting the same weight twice the distance.
Work is closely related to energy. The work-energy principle states that an increase in the kinetic energy of a rigid body is caused by an equal amount of positive work done on the body by the resultant force acting on that body. Conversely, a decrease in kinetic energy is caused by an equal amount of negative work done by the resultant force.
From Newton's second law, it can be shown that work on a free (no fields), rigid (no internal degrees of freedom) body, is equal to the change in kinetic energy of the velocity and rotation of that body.
Each delta v requires the same burn, not more to account for the fact that future fuel is more effective. The reason we don't see more paradoxes with rockets is that they require so much mass that they run out before that point would be reached and they are so very inefficient so most kinetic energy is wasted.
Also, I don't consider the energy issue a paradox if you use the work-energy theorem. It's the mechanical power times the time that always equates to the kinetic energy change in every observer frame. So there is no paradox. There is just a mixing of energy from different frames that confuses people.
...
How can acceleration be decreasing proportional to the speed? This would mean that acceleration would be measured differently in different frames of reference (i.e. it would have to be higher in a frame co-moving with the rocket w/o acceleration). How is that possible?
...
On the ship A = F/M rules. The energy / work required to be done on the constant mass of the ship to effect velocity change never varies. The ship doesn't care what some other frame calculates as the necessary energy to cause velocity change.
...
The Earth's frame only matters if an inbound ship needs to match velocity.
However the work needed to be done on the ship's mass to alter the relative velocity to 0, in the ship's frame, stays constant and that is the only effect that is important.