Jones:

Yes, even we vorticians have been jaded.  A claimed COP of 8 usually leads
to a tried & tested COP of 1.8 when all is said & done, and the error bars
typically are +/- 0.7, so it becomes unremarkable.

With that perspective an outset claimed COP of 1.68 usually leads to a
tried & tested COP of less than unity.

But I've seen electogravitics claims go black.  The entire field of
electrogravitics was classified in the 1950's.

Good enough place to start:
http://www.quantum-potential.com/ACT%20NASA.pdf

Kevin O




On Tue, Jul 29, 2014 at 8:07 AM, Jones Beene <jone...@pacbell.net> wrote:

>  Hi Kevin,
>
>
>
> This is from an older thread, but the comment did not get through.
>
>
>
> Basically, it is this. What is wrong with a COP of 1.68 on the early
> rounds of development of a new technology?
>
>
>
> It is almost as if Vortex, with all the claims floating around, has become
> jaded by expectation levels of COP which are unrealistic. I would love to
> see a Rossi device, or Mills device, or Mizuno device confirmed at COP
> 1.68, so long as this number was rock-solid … as in a rocket thruster,
> since there is more to the advantage than energy gain.
>
>
>
> Basically – Any confirmed OU level over 1 - would overturn about half of
> physics; and is up there with the most significant inventions of all time.
> And we have to assume that a first prototype of any thruster is below the
> eventual level. But anyway - for rocketry – NASA is not as concerned with
> OU as with
>
> “specific impulse”.
>
>
>
> The important figure of merit for this thruster then becomes:
>
>
>
> For the BLP Rocket engine, a maximum theoretical Isp of 21,000 seconds is
> predicted as compared to approximately 500
>
> seconds for an H2/O2 chemical rocket.
>
>
>
> That is huge. Of course, this “predicted” figure may contain the usual
> Mills hype, since the Rowan demo was not really “independent”. Mills and
> Janssen are reported to be personal friends.
>
>
>
> But with the possibility that the 40:1 thrust improvement (isp) when
> looked at in a finished rocket is only 4:1 improvement, in reality (i.e. if
> we reduce the BS level by a factor of 10) NASA should have stuck with this
> device IMO even if the COP was not extravagant.
>
>
>
> Hmm….Perhaps they did stick with it… and the project is now black. Black
> as in Morgan Freeman’s role in “Chain Reaction” … okay… that was only
> Hollywood and that kind of thing seldom happens, right …
>
>
>
> *From:* Kevin O'Malley
>
>
>
> COP was from 1.06 to 1.68.  No wonder they never pursued it.
>
>
>
>
> Take a close look at Janssen’s microwave thruster at Rowan – how could NASA 
> not
> have jumped on that?
>
>
>

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