Quote from: meberbs on 10/30/2016 08:36 PMQuote from: Bob012345 on 10/30/2016 05:45 PMNot the electrical power, the mechanical power which is F*v such that the thrust then remains constant.Some toy electric airplane motors deliver about 0.088N/W (27oz for 85W). Given an initial thrust of about 7.5N, the thrust doesn't diminish by a factor of 10 as the plane picks up speed of 10m/s then 20 as the speed gets to 20m/s. It's constant up to and at the equilibrium with the drag. But if the air had zero drag, the acceleration would be constant. The Shawyer probe is powered at about 200KW with about 30KW going to RF power. The Cannae probe has less than 100W RF power.No, the faster the plane is moving relative to the air, the more power it takes to accelerate the air to produce the same force. Drag is an additional effect. Doing the calculations in different frames (the rest frame of the air, or some other constant velocity frame) will all lead to the same conclusion that the power required to generate a constant force varies with the speed of the air relative to the plane. (which is independent of reference frame, because it is the difference of velocities, so all calculate the same power and force, and that power/ force varies with airspeed.)Example (using a discrete event instead of continuous to make it easier to follow, so energy (E) instead of power, change in momentum (Δp) instead of force. Subscript a means air, p means plane, 1 means initial, 2 means final.conservation of momentum:ma*va1 + mp*vp1 = ma*va2 + mp*vp2 Δp = -ma*(va2 - va1 ) = mp*(vp2 - vp1 )conservation of energy:0.5*ma*va12 + 0.5*mp*vp12 + E = 0.5*ma*va22 + 0.5*mp*vp22Rearrange to solve for E, group the terms, and apply a2-b2 = (a+b)(a-b) pull out the parts which are equal to Δp, and you get:E = 0.5*Δp*( (vp2 - va2) + (vp1 - va1) )Therefore, for a constant change in the plane's momentum, the engine needs to output more energy if the plane's airspeed is higher, and all frames agree on this amount of energy, since it comes from frame-independent potential energy (chemical/electrical).In any real system, there are many other complications (temperature changes, motor efficiency as function of RPM etc.), but this effect will still be there.No, the engine puts out a fixed power and thrust. The plane then accelerates to its max speed for that power and is in a steady state. It's all very simple but you're over complicating it. According to you, the thrust drops the instant the plane moves. Not true. But this isn't a perfect example since the air defines a fixed frame.
Quote from: Bob012345 on 10/30/2016 05:45 PMNot the electrical power, the mechanical power which is F*v such that the thrust then remains constant.Some toy electric airplane motors deliver about 0.088N/W (27oz for 85W). Given an initial thrust of about 7.5N, the thrust doesn't diminish by a factor of 10 as the plane picks up speed of 10m/s then 20 as the speed gets to 20m/s. It's constant up to and at the equilibrium with the drag. But if the air had zero drag, the acceleration would be constant. The Shawyer probe is powered at about 200KW with about 30KW going to RF power. The Cannae probe has less than 100W RF power.No, the faster the plane is moving relative to the air, the more power it takes to accelerate the air to produce the same force. Drag is an additional effect. Doing the calculations in different frames (the rest frame of the air, or some other constant velocity frame) will all lead to the same conclusion that the power required to generate a constant force varies with the speed of the air relative to the plane. (which is independent of reference frame, because it is the difference of velocities, so all calculate the same power and force, and that power/ force varies with airspeed.)Example (using a discrete event instead of continuous to make it easier to follow, so energy (E) instead of power, change in momentum (Δp) instead of force. Subscript a means air, p means plane, 1 means initial, 2 means final.conservation of momentum:ma*va1 + mp*vp1 = ma*va2 + mp*vp2 Δp = -ma*(va2 - va1 ) = mp*(vp2 - vp1 )conservation of energy:0.5*ma*va12 + 0.5*mp*vp12 + E = 0.5*ma*va22 + 0.5*mp*vp22Rearrange to solve for E, group the terms, and apply a2-b2 = (a+b)(a-b) pull out the parts which are equal to Δp, and you get:E = 0.5*Δp*( (vp2 - va2) + (vp1 - va1) )Therefore, for a constant change in the plane's momentum, the engine needs to output more energy if the plane's airspeed is higher, and all frames agree on this amount of energy, since it comes from frame-independent potential energy (chemical/electrical).In any real system, there are many other complications (temperature changes, motor efficiency as function of RPM etc.), but this effect will still be there.
Not the electrical power, the mechanical power which is F*v such that the thrust then remains constant.Some toy electric airplane motors deliver about 0.088N/W (27oz for 85W). Given an initial thrust of about 7.5N, the thrust doesn't diminish by a factor of 10 as the plane picks up speed of 10m/s then 20 as the speed gets to 20m/s. It's constant up to and at the equilibrium with the drag. But if the air had zero drag, the acceleration would be constant. The Shawyer probe is powered at about 200KW with about 30KW going to RF power. The Cannae probe has less than 100W RF power.
Quote from: wicoe on 10/31/2016 05:28 PMQuote from: Bob012345 on 10/31/2016 05:08 PMVelocity is relative but acceleration is absolute. Thus, if the EmDrive works, it produces a force and thus an acceleration regardless of anything. There is no way for it to "know" what velocity it's going such as to "know" it's kinetic energy is in danger of growing at a rate beyond which the power it is supplying can handle. The only limitation must be that the force it produces is proportional to the power it uses to produce that force.If the EmDrive works by "pushing" against something (i.e. some unknown field or other objects in the universe via gravity assist), it perfectly "knows" its velocity relative to the medium/objects it's pushing against. And just like with any other "pushing" mechanism, the higher your velocity, the harder it is to push. This is required for CoM/CoE to be observed, as has been explained multiple times in this thread.You've just defined a fixed absolute frame for the universe, something Relativity forbids. What would be required for CoM/CoE preservation is that the pushing is the same in all frames. In effect, every frame is equivalent and can be "pushed" against equally. Every frame of the universe must be the Center of Momentum frame.
Quote from: Bob012345 on 10/31/2016 05:08 PMVelocity is relative but acceleration is absolute. Thus, if the EmDrive works, it produces a force and thus an acceleration regardless of anything. There is no way for it to "know" what velocity it's going such as to "know" it's kinetic energy is in danger of growing at a rate beyond which the power it is supplying can handle. The only limitation must be that the force it produces is proportional to the power it uses to produce that force.If the EmDrive works by "pushing" against something (i.e. some unknown field or other objects in the universe via gravity assist), it perfectly "knows" its velocity relative to the medium/objects it's pushing against. And just like with any other "pushing" mechanism, the higher your velocity, the harder it is to push. This is required for CoM/CoE to be observed, as has been explained multiple times in this thread.
Velocity is relative but acceleration is absolute. Thus, if the EmDrive works, it produces a force and thus an acceleration regardless of anything. There is no way for it to "know" what velocity it's going such as to "know" it's kinetic energy is in danger of growing at a rate beyond which the power it is supplying can handle. The only limitation must be that the force it produces is proportional to the power it uses to produce that force.
Quote from: Bob012345 on 10/31/2016 04:16 PMQuote from: meberbs on 10/30/2016 08:36 PMQuote from: Bob012345 on 10/30/2016 05:45 PMNot the electrical power, the mechanical power which is F*v such that the thrust then remains constant.Some toy electric airplane motors deliver about 0.088N/W (27oz for 85W). Given an initial thrust of about 7.5N, the thrust doesn't diminish by a factor of 10 as the plane picks up speed of 10m/s then 20 as the speed gets to 20m/s. It's constant up to and at the equilibrium with the drag. But if the air had zero drag, the acceleration would be constant. The Shawyer probe is powered at about 200KW with about 30KW going to RF power. The Cannae probe has less than 100W RF power.No, the faster the plane is moving relative to the air, the more power it takes to accelerate the air to produce the same force. Drag is an additional effect. Doing the calculations in different frames (the rest frame of the air, or some other constant velocity frame) will all lead to the same conclusion that the power required to generate a constant force varies with the speed of the air relative to the plane. (which is independent of reference frame, because it is the difference of velocities, so all calculate the same power and force, and that power/ force varies with airspeed.)Example (using a discrete event instead of continuous to make it easier to follow, so energy (E) instead of power, change in momentum (Δp) instead of force. Subscript a means air, p means plane, 1 means initial, 2 means final.conservation of momentum:ma*va1 + mp*vp1 = ma*va2 + mp*vp2 Δp = -ma*(va2 - va1 ) = mp*(vp2 - vp1 )conservation of energy:0.5*ma*va12 + 0.5*mp*vp12 + E = 0.5*ma*va22 + 0.5*mp*vp22Rearrange to solve for E, group the terms, and apply a2-b2 = (a+b)(a-b) pull out the parts which are equal to Δp, and you get:E = 0.5*Δp*( (vp2 - va2) + (vp1 - va1) )Therefore, for a constant change in the plane's momentum, the engine needs to output more energy if the plane's airspeed is higher, and all frames agree on this amount of energy, since it comes from frame-independent potential energy (chemical/electrical).In any real system, there are many other complications (temperature changes, motor efficiency as function of RPM etc.), but this effect will still be there.No, the engine puts out a fixed power and thrust. The plane then accelerates to its max speed for that power and is in a steady state. It's all very simple but you're over complicating it. According to you, the thrust drops the instant the plane moves. Not true. But this isn't a perfect example since the air defines a fixed frame.Overcomplicating? I literally described the simplest ideal case of a vehicle pushing on a medium to accelerate, and showed that your assertion of fixed power for fixed thrust is false. Repeating your basic assertion that I just disproved shows a complete lack of comprehension on your part."According to you, the thrust drops the instant the plane moves." - No, not according to me. According to basic mechanics, as the plane's velocity relative to the air increases, either the generated force decreases, the power delivered to the motor increases, or something in between.Quote from: Bob012345 on 10/31/2016 05:37 PMQuote from: wicoe on 10/31/2016 05:28 PMQuote from: Bob012345 on 10/31/2016 05:08 PMVelocity is relative but acceleration is absolute. Thus, if the EmDrive works, it produces a force and thus an acceleration regardless of anything. There is no way for it to "know" what velocity it's going such as to "know" it's kinetic energy is in danger of growing at a rate beyond which the power it is supplying can handle. The only limitation must be that the force it produces is proportional to the power it uses to produce that force.If the EmDrive works by "pushing" against something (i.e. some unknown field or other objects in the universe via gravity assist), it perfectly "knows" its velocity relative to the medium/objects it's pushing against. And just like with any other "pushing" mechanism, the higher your velocity, the harder it is to push. This is required for CoM/CoE to be observed, as has been explained multiple times in this thread.You've just defined a fixed absolute frame for the universe, something Relativity forbids. What would be required for CoM/CoE preservation is that the pushing is the same in all frames. In effect, every frame is equivalent and can be "pushed" against equally. Every frame of the universe must be the Center of Momentum frame.You don't push against frames. If there is some medium that the emDrive pushes against (lets just say dark matter for now), than the work required to push against the dark matter depends on the relative velocity between the drive and the dark matter, which creates the "special frame" of the medium (the local dark matter rest frame) This kind of special frame is allowed by special relativity, just like the frame of the air is a special frame for an airplane.Your continued search for a better than photon rocket constant force/power system is getting tiring, since it has been shown multiple times and ways that this simply does not work in Newtonian Mechanics or special relativity.
Basically, your just saying EmDrive can't work so why discuss it. We discuss it because that's what thus thread is set up to discuss. I'm not the only one saying it might work and if it does, you will just have to change your perspective.It's already been proven that with photon recycling, better than a photon rocket is possible. The EmDrive seems to offer a potential billion times improvement over a photon rocket.
The basic point is that you say the EmDrive, if it works at all, will stop accelerating as it's kinetic energy grows faster than its electrical energy input. You're claiming you know Shawyer, Fetta and anyone else who shows a fixed thrust for a fixed electrical power doesn't understand how physics works if they claim that acceleration will just continue. Myself and others believe if it works at all, nothing can limit the acceleration since all observer frames are arbitrary. I believe the energy conundrum is only an apparent violation. Velocity is relative but acceleration is absolute. Thus, if the EmDrive works, it produces a force and thus an acceleration regardless of anything. There is no way for it to "know" what velocity it's going such as to "know" it's kinetic energy is in danger of growing at a rate beyond which the power it is supplying can handle. The only limitation must be that the force it produces is proportional to the power it uses to produce that force which is the point Woodward made.
...Now in late 2016 Roger has released a radical cryo EmDrive, that based on the cavity TC from the Force generation curves, would have a Ql of ~3x10^9 and specific force of ~10,000N/kWrf. Seems Roger has been busy.Several here have stated YBCO will not work at microwave frequencies. Seems their opinion may need to be updated.143kg/6kWrf is a specific force of 234N/kWrf which is not that far above the 145N/kWrf figure for LHe cooling of the Experimental cryo EmDrive data.
Quote from: PotomacNeuron on 10/31/2016 01:40 PMQuote from: TheTraveller on 10/31/2016 11:26 AMInteresting data from Roger's 2009 paper on his Experimental YBCO thruster where he published experimentally measured surface resistance data for YBCO on Sapphire data at 3.83GHz. He also stated the experimentally measured Qu was 6.8x10^6, cooled with LN2, which would produce a specific force of 41N/kWrf, increasing to 145N/kWrf if cooled by LHe.I then plotted the results for cooling with LH2 and LHe as attached.He further states in the paper that the data was from his 1st Experimental cryo EmDrive and that he has moving to build a Demonstrator EmDrive, following the development process and names of the non cryo EmDrives. That was in 2009. Now in late 2016 Roger has released a radical cryo EmDrive, that based on the cavity TC from the Force generation curves, would have a Ql of ~3x10^9 and specific force of ~10,000N/kWrf. Seems Roger has been busy.Several here have stated YBCO will not work at microwave frequencies. Seems their opinion may need to be updated.143kg/6kWrf is a specific force of 234N/kWrf which is not that far above the 145N/kWrf figure for LHe cooling of the Experimental cryo EmDrive data.Would you please make it clear that the "41N/kWrf", "145N/kWrf", "~10,000N/kWrf", "143kg/6kWrf", "234N/kWrf" are all speculated based on Q and are not actually measured? I think many may not read carefully enough and may get incorrect impression.The Qu of 6.8x10^6 and Rs of 78 uOhm for the YBCO on Sapphire thin film at 77K and 3.83GHz are experimentally measured values.There are established equations that link the other values together. One follows the other as does Ohm's law. Shall I then question every Ohm's law calculation because it has not been experimentally measured?Roger measured the Qu in his 1st experimental YBCO EmDrive and then measured the surface resistance change vs temp at 3.82GHz. It is simple math to do the calc at other values of Rs once the Qu vs Rs at one temp is known.This is known as EmDrive Engineering 101.
Quote from: TheTraveller on 10/31/2016 11:26 AMInteresting data from Roger's 2009 paper on his Experimental YBCO thruster where he published experimentally measured surface resistance data for YBCO on Sapphire data at 3.83GHz. He also stated the experimentally measured Qu was 6.8x10^6, cooled with LN2, which would produce a specific force of 41N/kWrf, increasing to 145N/kWrf if cooled by LHe.I then plotted the results for cooling with LH2 and LHe as attached.He further states in the paper that the data was from his 1st Experimental cryo EmDrive and that he has moving to build a Demonstrator EmDrive, following the development process and names of the non cryo EmDrives. That was in 2009. Now in late 2016 Roger has released a radical cryo EmDrive, that based on the cavity TC from the Force generation curves, would have a Ql of ~3x10^9 and specific force of ~10,000N/kWrf. Seems Roger has been busy.Several here have stated YBCO will not work at microwave frequencies. Seems their opinion may need to be updated.143kg/6kWrf is a specific force of 234N/kWrf which is not that far above the 145N/kWrf figure for LHe cooling of the Experimental cryo EmDrive data.Would you please make it clear that the "41N/kWrf", "145N/kWrf", "~10,000N/kWrf", "143kg/6kWrf", "234N/kWrf" are all speculated based on Q and are not actually measured? I think many may not read carefully enough and may get incorrect impression.
Interesting data from Roger's 2009 paper on his Experimental YBCO thruster where he published experimentally measured surface resistance data for YBCO on Sapphire data at 3.83GHz. He also stated the experimentally measured Qu was 6.8x10^6, cooled with LN2, which would produce a specific force of 41N/kWrf, increasing to 145N/kWrf if cooled by LHe.I then plotted the results for cooling with LH2 and LHe as attached.He further states in the paper that the data was from his 1st Experimental cryo EmDrive and that he has moving to build a Demonstrator EmDrive, following the development process and names of the non cryo EmDrives. That was in 2009. Now in late 2016 Roger has released a radical cryo EmDrive, that based on the cavity TC from the Force generation curves, would have a Ql of ~3x10^9 and specific force of ~10,000N/kWrf. Seems Roger has been busy.Several here have stated YBCO will not work at microwave frequencies. Seems their opinion may need to be updated.143kg/6kWrf is a specific force of 234N/kWrf which is not that far above the 145N/kWrf figure for LHe cooling of the Experimental cryo EmDrive data.
Quote from: zen-in on 10/31/2016 02:00 PMIn Shawyer's paper he states the surface resistivity data is "based on specified manufacturer's data" (quoted from his paper). In all probability he does not possess any of the sapphire substrate HTS described in his paper and he has not built the device you describe as "an experimental HTS thruster" There are thousands of papers published every year devoted to esoteric measurements of small sections of HTS in carefully controlled laboratory setups. Shawyer has extrapolated from that with his claim an HTS em-drive thruster is possible and you have taken a much bigger leap by claiming he has built "an experimental HTS thruster".He states he built an Experimental cryo YBCO on Sapphire EmDrive thruster. Even shared a photo.Minus the 2 images (Fig 12 and Fig 13) here is what Roger wrote:Quote7.SUPERCONDUCTING DEMONSTRATOR PROGRAMMEThe first phase of this programme was an experimental superconducting thruster. This low power, HTS device operates at liquid nitrogen temperature, and is designed for very high Q and consequently high specific thrust.Fig 12 Experimental Superconducting Thruster as attachedFig 12 shows the thruster, which operates at 3.8 GHz, and was designed using an update of the software used for the previous S band designs. Super-conducting surfaces are formed from YBCO thin films on sapphire substrates.Small signal testing at 77 deg K confirmed the design, with a Q of 6.8x10^6 being measured.Fig 13 shows the surface resistivity of the superconducting thruster based on specified manufacturer’s data, updated for the measured data. Fig 13 Surface Resistivity as attached.For the Demonstrator Thruster, cooling will be by liquid hydrogen. The design resistivity at 20deg K is therefore taken as 11.8 x 10-6 Ohms. This value was then used in the same design software used for the experimental 2G thruster. The resulting thrust was calculated as 143kg for 6kW input.
In Shawyer's paper he states the surface resistivity data is "based on specified manufacturer's data" (quoted from his paper). In all probability he does not possess any of the sapphire substrate HTS described in his paper and he has not built the device you describe as "an experimental HTS thruster" There are thousands of papers published every year devoted to esoteric measurements of small sections of HTS in carefully controlled laboratory setups. Shawyer has extrapolated from that with his claim an HTS em-drive thruster is possible and you have taken a much bigger leap by claiming he has built "an experimental HTS thruster".
7.SUPERCONDUCTING DEMONSTRATOR PROGRAMMEThe first phase of this programme was an experimental superconducting thruster. This low power, HTS device operates at liquid nitrogen temperature, and is designed for very high Q and consequently high specific thrust.Fig 12 Experimental Superconducting Thruster as attachedFig 12 shows the thruster, which operates at 3.8 GHz, and was designed using an update of the software used for the previous S band designs. Super-conducting surfaces are formed from YBCO thin films on sapphire substrates.Small signal testing at 77 deg K confirmed the design, with a Q of 6.8x10^6 being measured.Fig 13 shows the surface resistivity of the superconducting thruster based on specified manufacturer’s data, updated for the measured data. Fig 13 Surface Resistivity as attached.For the Demonstrator Thruster, cooling will be by liquid hydrogen. The design resistivity at 20deg K is therefore taken as 11.8 x 10-6 Ohms. This value was then used in the same design software used for the experimental 2G thruster. The resulting thrust was calculated as 143kg for 6kW input.
Surface resistivity measurements at microwave frequencies are high when compared to the DC resistance of superconductors. These measurements are done with very low RF power levels. Higher RF power would introduce self heating from the RF losses destroying the superconductivity. Superconductor physics is a lot more complicated than simply applying Ohm's law to one or two points and extrapolating.
I caught some flack for making Q a variable of the coordinates inside the frustum. So here are the thrust and group velocity equations using the damping factor instead, which is an acceptable variable function of the coordinates inside the frustum. Now, the thrust is proportional to Q, but it is also proportional to the 4-gradient of the damping potential.Todd
......Thrust force is a static force that can be measured on a scale or torsion pendulum, is there all the time there is resonant Rf in the cavity and doesn't need free acceleration to be measured......
Quote from: TheTraveller on 11/01/2016 06:05 AM......Thrust force is a static force that can be measured on a scale or torsion pendulum, is there all the time there is resonant Rf in the cavity and doesn't need free acceleration to be measured......You come up again with that concept of 'force-less free acceleration'. I believe Shawyer also talks about it. It would be the most revolutionary thing to emerge from the EMdrive, doesn't it? To me it merely sounds like an excuse to explain null-results of experiments. Even gravitation acts as a force. It is very hard to imagine what the nature of such a 'force-free acceleration' would be.Cheers, Peter
Quote from: Peter Lauwer on 11/01/2016 07:45 AMQuote from: TheTraveller on 11/01/2016 06:05 AM......Thrust force is a static force that can be measured on a scale or torsion pendulum, is there all the time there is resonant Rf in the cavity and doesn't need free acceleration to be measured......You come up again with that concept of 'force-less free acceleration'. I believe Shawyer also talks about it. It would be the most revolutionary thing to emerge from the EMdrive, doesn't it? To me it merely sounds like an excuse to explain null-results of experiments. Even gravitation acts as a force. It is very hard to imagine what the nature of such a 'force-free acceleration' would be.Cheers, PeterThe EmDrive generates 2 forces:1) Static Thrust force which is generated by the guide wavelength variation with changing cavity diameter. The Thrust force vector follows longer guide wavelength to shorter guide wavelength direction in the resonant cavity. In a non dielectric cavity, the Thrust force vector is small to big end. It has been measured by many experimenters using a scale or a torsion pendulum, which is just a fancy scale. No movement of the cavity is required for the Thrust force to be generated. Well Ok a little movement happens as all scale like devices have a spring constant.2) Accelerative Reaction force, which is equal in value but opposite in force vector to the Thrust force. It can only be measured via A = F/M on a rotary test rig or linear test rig that allows free acceleration to occur.Most EmDrive experimenters measure the static Thrust force.I know of only 2 EmDrive experiments that have measured the accelerative Reaction force. One being Roger's 2006 Demonstrator testing on a rotary air bearing test rig and another that I can't share but has very high credibility. I'm working to make that 3.Both of these forces can and have been measured, but not at the same time, including the Thrust force vector change that happens when you add a dielectric to the small end of the cavity.Now we need a theory that predicts what has been physically measured. So far Roger's is the closest I know of.
But it certainly a good thing that there are 'believers' (excusez le mot) and sceptics on this forum! We should not avoid though discussions. (when I started to set up a replication experiment I was for 99.9% certain it was all due to heat effects and magnetic fields, etc. Now I would set that to 90%. So my believe in the possibility that there really is an anomalous effect already increased 100-fold!). '-)Keep up the good work.Peter
....But it certainly a good thing that there are 'believers' (excusez le mot) and sceptics on this forum! We should not avoid though discussions. (when I started to set up a replication experiment I was for 99.9% certain it was all due to heat effects and magnetic fields, etc. Now I would set that to 90%. So my believe in the possibility that there really is an anomalous effect already increased 100-fold!). '-)Keep up the good work.Peter
Very soon I trust that will be 0% doubt.