[AR] Re: NASA test of quantum vacuum plasma thruster (was "Anyone heard of this?")

  • From: Jake Anderson <jake@xxxxxxxxxxxxxxx>
  • To: arocket@xxxxxxxxxxxxx, Joel Brinton <jdbrinton@xxxxxxxxx>
  • Date: Mon, 04 Aug 2014 18:47:15 +1000

I do like the idea of the test being done in basically a clear bell jar inside a (large) Faraday cage. I also like the pendulum, however I'm less keen on the piezo pressure sensor.

I suggest a laser interferometer aimed at the pendulum.

If you want to verify thrust in a direction put 2 test devices on it, have the oppose each other, turn one on you should get a displacement in one direction, turn it off you should return to zero, turn the other on displacement in the opposite direction, you don't need to make any changes inside the test device to perform the test which is nice.

For extra credit power the thing by battery on the rig itself so there are no penetrations through the jar, the whole thing can be totally isolated.

On 03/08/14 15:06, Michael Clive wrote:

I bought the paper. I personally don't care about the physics of how it works YET.

All I care about is verifying if it works.
So I am gonna build one.
Here is where yall come in.

Let us define what would be a two factor test for this. I want two high accuracy sensors to measure force. I am thinking a diaphragm backed by an ultra high accuracy pizeo pressure transducer, an lvdt to measure displament against the diaphragm and possibly a laser interferometer for measuring distance.

Background on me: I work at spacex, used to work at xcor, I live in a giant warehouse with three phase power. I am on first name basis with half the machine shops in los angeles. I build test systems everyday all day. Never done microwaves before but I am a quick learner.

What I need from the people on this list is help on design for an ultra sensitive verification system. Then I will start a kickstarter, collect the fifty grand or so from the cloud, and build the thing. I will build it in a portable self contained unit. I will run the first batch of experiments. If there are positive results, I will freely hand it off to the first university that wants to play with it, and so on. If there are negative results, I want to make sure I am the one to put a bullet in this things head.

Why do I want to do this? This would change the entire game as far as mars colonization and settlement is concerned. Also, I have many of the required skills to build test and verification equipment, and I am perfectly willing to accept a negative result.

If anyone wants to team up, I am based out of los angeles.

Here is what I need
1. A primary way to verify operation or non operation of the device, by direct force measument.
2. A secondary indirect system to verify the device.
3. A tertiary analog system to rule out electro magnetic interference.
4. An electrical engineer to help
5. An RF engineer to help. Jb plz
6. Money. Which I will try to kick start cloudfund after I work out a budget for this.

Goal is to have a running test bed by January.

The paper is pretty clear on expemient setup. If we triple down on verification systems, I think we can nail this to a wall, one way or another.

Who's with me?

On Aug 2, 2014 5:09 PM, "Ian Woollard" <ian.woollard@xxxxxxxxx <mailto:ian.woollard@xxxxxxxxx>> wrote:

    There's essentially no chance that a thruster can work where you
    turn it on, feeding only electricity through it, and with nothing
    leaving it; where you switch it off, and you're now moving faster.
    This is what the emdrive is claimed to do.

    If you could do that, we're in perpetual motion territory; because
    it violates both conservation of momentum, and (more subtly) it
    can be shown to violate conservation of energy.

    The emdrive paper tried to fix that by using the kinetic energy
    equation in one frame of reference, but you can show that energy
    is violated in every other frame of reference except the one he
    did the calculation in. So he's done something wrong. You can fix
    it, if you introduce an efficiency variable, and set the variable
    to zero.

    On 2 August 2014 23:44, Willow Schlanger <wschlanger@xxxxxxxxx
    <mailto:wschlanger@xxxxxxxxx>> wrote:

        I just bought the AIAA paper (it's a 21 page PDF) from this
        location:
        http://arc.aiaa.org/doi/abs/10.2514/6.2014-4029

        I also discovered I have an old paper on the EmDrive from
        "Satellite
        Propulsion Research Ltd." The filename is "theory paper
        V9.3.doc" and I
        received it September 16, 2006 from (if I remember correctly)
        Roger
        Shawyer. Here is the first sentence from the Abstract: "A new
        principle
        of electric propulsion for spacecraft is introduced, using
        microwave
        technology to achieve direct conversion of d.c. power to
        thrust without
        the need for propellant."

        It's been a while since I've read that paper (and I'm
        surprised I was
        able to find a copy of it saved from all those years ago), but
        I don't
        think it mentioned anything quantum related. I'm taking a
        quick look; I
        think he attempted to use only special relativity and non-quantum
        physics to describe the effect.

        I'm not sure I'll be able to figure out what any of this
        means, but I'll
        try to do some reading and post my thoughts here, if I can
        decipher what
        they're all talking about. The AIAA paper was $25.00, and the old
        "theory paper" mentioned above was sent to me back in 2006 for
        free (but
        both documents are copyrighted so I can't share them).

        Willow Schlanger


        On Sat, Aug 2, 2014 at 1:26 PM, Satadru Pramanik
        <satadru@xxxxxxxxx <mailto:satadru@xxxxxxxxx>> wrote:

            There's some discussion of the merits of this paper on
            reddit by this user here:

            http://www.reddit.com/user/dalovindj

            He says that the null article wasn't a control, but used
            to test under which conditions the effect occurred:

            "The null configuration (not the RF load - not the control
            but the/central/subject of a test) was one of two test
            articles. There are two competing theories as to how the
            phenomenon works. Fetta believes that it works based on
            asymmetry in the design, while White believes it works by
            pushing against the quantum vacuum.

            They tested an asymetric and a symetric design. The
            symmetric design (neither were "broken") is what they
            refer to as the null. It was meant to test a prediction of
            Fetta's theory on how the device produces thrust. He
            believes that the force is produced by an imbalance of the
            lorentz force caused by the asymmetric chamber. This test
            seems to indicate that Fetta's theory is incorrect (or at
            the very least innacurate). Dr. White's theory on how
            thrust is produced (pushing against the quantum vacuum),
            however, predicted that both test articles should produce
            thrust, which they did. It would seem an endorsement of
            White's theory over Fetta's."



            This is stated in the paper as such:

            Prior to testing, Cannae theorized that the asymmetric
            engraved slots would result in a force imbalance (thrust).
            As a result, a second (control) test article was
            fabricated without the internal slotting (a.k.a. the null
            test article).


            Let me know if anybody wants a copy of the paper.
             Seriously discussing the merits of the physics in this
            paper is currently above my pay grade.



            On Sat, Aug 2, 2014 at 11:15 AM, David Weinshenker
            <daze39@xxxxxxxxxxxxx <mailto:daze39@xxxxxxxxxxxxx>> wrote:

                William Blair (Redacted sender wbblair3@xxxxxxxxx
                <mailto:wbblair3@xxxxxxxxx> for DMARC) wrote:
                > How could they then be certain that air movement
                caused by the differential heating
                > of the air within the RF cavity hadn't caused the
                measured micro-thrust? I must be
                > missing something because this seems to be too
                obvious of a potential flaw in the test.

                Well, the abstract (is the full text available
                anywhere?) did mention a comparison
                run they did with an "RF load" replacing the test
                device, which seems to be intended
                to control for effects such as you suggest. (If the
                test device wasn't designed and
                baked out for operation in vacuum, escaping air from
                crevices, and outgassing of
                surfaces, could conceivably create spurious forces of
                their own if the chamber was
                pumped down to vacuum.)

                -dave w






-- -Ian Woollard


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