Thanks so much for this review. I was very excited, obviously, about this, but upon reflection and the wisdom of people such as you, I have gained a better handle on the experiment. As someone who runs a test facility and often sees people screw up data because they are not familiar with the equipment, your review rings very true. Dang. Too bad. Now I feel silly for getting all enthusiastic about this. On Mon, Aug 4, 2014 at 7:38 PM, Willow Schlanger <wschlanger@xxxxxxxxx> wrote: > Hi John, > Thanks for this review; it's a great wake-up call from someone who > really read the paper. So, back to reality for us "space cadets," then? > > Willow Schlanger > > On 08/04/2014 07:10 PM, John Schilling wrote: > > I was actually at that conference; didn't want to comment until I > > had a chance to read the paper, but now I have so here goes: > > > > The team appears to have used a standard NASA-Lewis torsion balance > > thrust stand. That thrust stand, which I have used extensively, is > > good to about +/- 10 microNewtons when used in the steady-state > > mode by an expert team. There is a resonant mode (look for a paper > > by Lake and Dulligan) that can get down to +/- 1 uN or better, but > > that isn't what was used here. > > > > Nor does the team that did this work appear to be thrust-stand > > experts. There is relatively little discussion of that aspect of > > their work, and what there is suggests that they did some things > > right (e.g. comparison to a ballast load to rule out interference > > from the power supply) and some things wrong (e.g. only a single-point > > calibration). They do not cite a reference to their thrust measurement > > technique, they do not give acknowledgement to any of the technicians, > > and a quick literature search of their prior work does not suggest > > great experience with the NASA-Lewis torsion balance thrust stand. > > Absent such expertise, or even the recognition that such expertise > > is necessary, errors of several tens of microNewtons are likely and > > hundreds of microNewtons are not implausible. > > > > One thing they unambiguously did right, was to test the null-hypothesis > > model of their "Cannae" thruster. Theory says that that with the > > asymmetric groves you get ~10,000 microNewtons of thrust from 28 Watts > > of electric power and without the groves you get zero thrust. They > > tested both, on a thrust stand with error bars of a few tens of > > microNewtons, and got ~50 microNewtons of indicated thrust. > > > > And made essentially no mention of this ever again, except to say > > "We got Thrust! Yay Us!". > > > > Their subsequent testing of the truncated-cone thruster conspicuously > > failed to make use of a null-hypothesis model. After repeatedly > > showing about the same (lack of) performance as the "Cannae" thruster > > in its first two operating modes, they conducted one single test of > > the truncated-cone thruster in a third operating mode, demonstrated a > > fivefold increase in thrust:power, and found that time and facility > > limitations meant they had to terminate the experiments. > > > > Finally, they put forth a batch of conclusions that are entirely > > unsupported by their own experimental data. It would have been bad > > enough to have reported the single anomalously high truncated-cone > > data point as the baseline and buried the null-hypothesis results. > > Worse, is reporting only the Chinese experimental results (nearly > > two orders of magnitude better than their own) and the theoretical > > calculations which they did not perform and did explicitly disclaim > > as beyond the scope of their paper, note that theory and experiment > > (other people's) indicate a thrust:power ratio of 0.4 N/kW, and > > proclaiming, "...and we also measured (mumble) thrust, so it's all > > true and we can have manned missions to the outer solar system any > > time now!" > > > > > > They measured experimental error, and nothing more. And they set the > > bar so low, with such implied authority, that we can now look forward > > to years of dueling claims of "I built an EMdrive out of spare parts > > and put it on a thrust stand I had lying around, and got microNewtons > > of thrust just like NASA!", "So did I, and I got nothing at all!" > > Did so, did not, ad infinitum. > > > > If theory and Chinese experiment really do validate claims of 0.4 N/kW, > > then you really can build an enclosed metal box (batteries in the box, > > to deal with the power-supply interactions Henry correctly notes) that > > will visibly tilt a straight hanging pendulum. Do that, and get back > > to us. > > > > Oh, and if you can build a reactionless thruster with a thrust:power > > ratio of 0.4 N/kW and can't think of anything better to do with it > > than fly to Uranus, you are an insanely myopic space cadet. I will > > leave it as an exercise to the student how one would incorporate such > > devices into a perpetual motion machine capable of providing clean, > > free energy on a massive scale. It isn't trivially easy, but it is > > almost certainly worth doing long before you build spaceships - and > > this was presented at a "Propulsion and Energy" conference, so it > > probably would have been worth mentioning. > > > > Well, except for the fact that the Energy attendees would have been > > more merciless in their heckling; there's a long tradition of tolerance > > in the "future flight" sessions of the AIAA Propulsion conferences. > > > > John Schilling > > john.schilling@xxxxxxxxxxxxxx > > (661) 718-0955 > > > > > >> Date: Sun, 03 Aug 2014 07:53:24 -0700 > >> From: Henry Vanderbilt<hvanderbilt@xxxxxxxxxxxxxx> > >> Subject: [AR] Re: NASA test of quantum vacuum plasma thruster (was > >> "Anyone > >> > >> G. Harry Stine made a sideline of looking into alleged reactionless > >> drives. He knew how incredibly useful such a thing would be, he really > >> wanted some such thing to be practical, so (typical of the man) he was > >> rigorously skeptical. I went along for the ride on at least one of his > >> visits, to a local guy who was trying to produce thrust mechanically. > >> (As usual, strange things happened when you turned the rpm high enough > >> just before the device flew apart, and as usual, there was no actual > >> thrust involved.) > >> > >> Harry was actually very kind and polite in letting the guy know it > >> wasn't real. Again, typical of the guy. > >> > >> (Enough reminiscing, cut to the chase.) I recall Harry explaining that > >> he considered a convincing demo to be: Hang the device on the end of a > >> pendulum in a vacuum, and demonstrate a repeatable constant displacement > >> of the pendulum with power on versus power off. > >> > >> And it occurs to me to add, twenty years later, since presumably power > >> of some sort is being routed to the device down the pendulum, set things > >> up so the device can be reoriented relative to the pendulum and power > >> feed, to distinguish between pendulum displacement due to the device > >> actually thrusting along some axis, and pendulum displacement due to > >> some power-on mechanical reaction of the power feed. > >> > >> Henry > > > > > > > > > >