I received the following message from Robert Ludwick answering Ron Stahl's comments:
From: Robert Ludwick
Sent: Friday, November 14, 2014 6:15 PM
To: Dr. J. Rodal
Subject: Testing the EmDrive
Hello Dr. Rodal,
This is in response to Ron Stahl's comments:
I think he’s right. He doesn’t understand. This is a very high Q resonator. The higher the Q, the narrower the bandwidth it can resonate at. Without resonance the Q will drop off to between 1/100 and1/10,000 what it is normally. The resonator needs to resonate. You cannot simply sweep a resonator and think you are changing the frequency only, when the Q is only for small bandwidths of specific frequencies.
Of course the higher the Q the narrower the bandwidth. Actually, Bandwidth=(resonant frequency)/Q ,so if we are talking frequencies of 1-2 Ghz and Q’s of (using Ron’s numbers above) 10,000 it implies a bandwidth of 100-200 KHz, which is NOT particularly narrow. Shawyer is talking superconducting thrusters with Q’s in the vicinity of 1e9. That would imply bandwidths of 1-2 Hz at the frequencies of the thrusters tested to date.
The test procedure I provided ASSUMED that a network analyzer had been used to identify the resonant frequencies and bandwidths of interest PRIOR to the start of the actual thrust test, so that the operator would be able to select appropriate start and stop frequencies, guaranteeing that the testing starts and stops well outside the high Q region and steps at the appropriate increment to ensure that there will be multiple thrust tests across the actual bandwidth of highest Q. The procedure ENSURES that the thruster is tested at the frequency of maximum Q, and thus, per theory, the frequency of maximum thrust. If any.
Then Ron Stahl states this:
Since Eagle has a PLL resonance matching circuit, there is little trouble with this except that you need to note you have not one but two variables as you have changed the amount of active mass.
First, please tell me that a lab set up to evaluate ‘Propellant-Less (exotic physics) Drives’ is NOT using a Mini-Circuits VCO, stabilized by a home brew Phase Locked Loop (PLL), as their lab signal source.
Concerning Ron's statement
….you need to note that you have not one but two variables, as you have changed the amount of active mass.
If you identify the frequency of maximum Q, then step the signal generator frequency through the frequency of maximum Q, holding the amplifier power constant, making sure you start well below the frequency of peak Q and stop well above it, using frequency steps small enough to ensure that at least 10 (and in the case of Q’s as low as 10,000, as many as 100) test frequencies are within the resonant bandwidth, and wait after each frequency step long enough for the mechanical system to stabilize before taking a thrust reading, how is that 'changing the active mass’ (using the definition of mass generally accepted in academia) ? If they are changing the internals of the thruster between tests, it would be necessary to put the thruster on the network analyzer after every ‘change of guts’ to identify the new resonant frequencies / bandwidths, but otherwise it would seem to me that the test as described would work just fine, and would only involve changing one factor: test frequency. Power and thus amplifier current would remain constant for the duration of the test. The purpose of the test is to discover if thrust is generated under any conditions and whether the thrust is related to the thruster Q at the drive frequency.
Then Ron Stahl states this:
This is much more difficult and much more expensive than you understand. Just the high speed auto matcher used up at George Hathaway’s lab cost $150k. And make no mistake, it is the power equipment that one presumes should be easy enough to build that costs so much. It was a big breakthrough for Eagle to get their PLL circuit in place and this is something that Woodward has never been able to do.
I have no idea what a ‘high speed auto matcher' is in this context, what function it performs, or why it is required to measure the thrust of an EmDrive. As for the PLL circuit is their need for something uniquely different from the standard use of PLL’s, which is to provide precisely controlled, stable outputs from an oscillator ?. And the ‘power equipment that costs so much’?? Again, what I have seen on the forum refers to amplifiers in the 1-3 GHz range that output a few tens of watts. THOSE are NOT expensive. So what is the super expensive ‘power equipment’ that Ron is talking about?
My simple minded interpretation of the commentary leads me to believe that Eagleworks could use some decent test equipment, such as signal sources, network analyzers, power meters, power amplifiers etc.
It is obvious from the over 200 pages of commentary on this subject I am not the only one excited about the claims about EM Drives. These folks need to get off the dime and get this thing going (or prove conclusively that there ain’t no there there, so I can relax and forget it).
Bob Ludwick