Plasma Aircraft/Spacecraft Technology

Beyond the boundaries of established science an avalanche of exotic ideas compete for our attention. Experts tell us that these ideas should not be permitted to take up the time of working scientists, and for the most part they are surely correct. But what about the gems in the rubble pile? By what ground-rules might we bring extraordinary new possibilities to light?

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Plasma Aircraft/Spacecraft Technology

Post by junglelord » Mon Apr 07, 2008 8:07 am

I will use this thread to try to recover several lost threads on plasma and aircraft.
The first deals with Stealth Technology and Plasma Aircraft.

Plasma stealth is a proposed process that uses ionized gas (plasma) to reduce the radar cross section (RCS) of an aircraft. Interactions between electromagnetic radiation and ionized gas have been extensively studied for a variety of purposes, including the possible concealment of aircraft from radar that plasma stealth theorizes. While it is theoretically possible to reduce an aircraft's RCS by wrapping the airframe in plasma, it may be very difficult to do so in practice. Various methods might plausibly be able to produce a layer or cloud of plasma around an airframe, from "simple" electrostatic or RF discharges to more exotic possibilities like laser-produced plasmas [1].

Despite the apparent technical difficulty of designing a plasma stealth device for combat aircraft, there are claims that a system was offered for export by Russia in 1999. In January of 1999, the Russian ITAR-TASS news agency published an interview with Doctor Anatoliy Koroteyev, the director of the Keldysh Research Center (FKA Scientific Research Institute for Thermal Processes), who talked about the plasma stealth device developed by his organization. The claim was particularly interesting in light of the solid scientific reputation of Dr. Koroteyev and the Institute for Thermal Processes, which is one of the top scientific research organizations in the world in the field of fundamental physics. [see "Russian scientists created revolutionary technologies for reducing radar visibility of aircraft", by Nikolay Novichkov, ITAR-TASS, January 20, 1999].

The Journal of Electronic Defense reported that "plasma-cloud-generation technology for stealth applications" developed in Russia reduces an aircraft's RCS by a factor of 100. According to this June 2002 article, the Russian plasma stealth device has been tested aboard a Sukhoi Su-27IB fighter-bomber. The Journal also reported that similar research into applications of plasma for RCS reduction is being carried out by Accurate Automation Corporation (Chattanooga, Tennessee) and Old Dominion University (Norfolk, Virginia) in the U.S.; and by Dassault Aviation (Saint-Cloud, France) and Thales (Paris, France). ["Russia Working on Stealth Plasma", by Michal Fiszer and Jerzy Gruszczynski, Journal of Electronic Defense, June 2002].

Plasmas on aerodynamic surfaces
Plasma layers around aircraft have been considered for purposes other than stealth. There are many research papers on the use of plasma to reduce aerodynamic drag. In particular, electrohydrodynamic coupling can be used to accelerate air flow near an aerodynamic surface. One paper[2] considers the use of a plasma panel for boundary layer control on a wing in a low-speed wind tunnel. This demonstrates that it is possible to produce a plasma on the skin of an aircraft. However, it is not clear whether the plasmas generated in these aerodynamics experiments could be used to reduce radar cross-section.


[edit] Absorption of EM radiation
When electromagnetic waves, such as radar signals, propagate into a conductive plasma, ions and electrons are displaced as a result of the time varying electric and magnetic fields. The wave field gives energy to the particles. The particles generally return some fraction of the energy they have gained to the wave, but some energy may be permanently absorbed as heat by processes like scattering or resonant acceleration, or transferred into other wave types by mode conversion or nonlinear effects. A plasma can, at least in principle, absorb all the energy in an incoming wave, and this is the key to plasma stealth. However, plasma stealth implies a substantial reduction of an aircraft's RCS, making it more difficult (but not necessarily impossible) to detect. The mere fact of detection of an aircraft by a radar does not guarantee an accurate targeting solution needed to intercept the aircraft or to engage it with missiles. A reduction in RCS also results in a proportional reduction in detection range, allowing an aircraft to get closer to the radar before being detected.

The central issue here is frequency of the incoming signal. A plasma will simply reflect radio waves below a certain frequency (which depends on the plasma properties). This aids long-range communications, because low-frequency radio signals bounce between the Earth and the ionosphere and may therefore travel long distances. Early-warning over-the-horizon radars utilize such low-frequency radio waves. Most military airborne and air defense radars, however, operate in the microwave band, where many plasmas, including the ionosphere, absorb or transmit the radiation (the use of microwave communication between the ground and communication satellites demonstrates that at least some frequencies can penetrate the ionosphere). Plasma surrounding an aircraft might be able to absorb incoming radiation, and therefore prevent any signal reflection from the metal parts of the aircraft: the aircraft would then be effectively invisible to radar. A plasma might also be used to modify the reflected waves to confuse the opponent's radar system: for example, frequency-shifting the reflected radiation would frustrate Doppler filtering and might make the reflected radiation more difficult to distinguish from noise.

Control of plasma properties is likely to be important for a functioning plasma stealth device, and it may be necessary to dynamically adjust the plasma density, temperature or composition, or the magnetic field, in order to effectively defeat different types of radar systems. Radars which can flexibly change their transmission frequency might be less susceptible to defeat by plasma stealth technology. Like LO geometry and radar absorbent materials, plasma stealth technology is probably not a panacea against radar.

Plasma stealth technology also faces various technical problems. For example, the plasma itself emits EM radiation. Also, it takes some time for plasma to be re-absorbed by the atmosphere and a trail of ionized air would be created behind the moving aircraft. Thirdly, plasmas (like glow discharges or fluorescent lights) tend to emit a visible glow: this is not necessarily compatible with overall low observability. Furthermore, it is likely to be difficult to produce a radar-absorbent plasma around an entire aircraft traveling at high speed. However, a substantial reduction of an aircraft's RCS may be achieved by generating radar-absorbent plasma around the most reflective surfaces of the aircraft, such as the turbojet engine fan blades, engine air intakes, and vertical stabilizers.

http://en.wikipedia.org/wiki/Plasma_stealth
If you only knew the magnificence of the 3, 6 and 9, then you would have a key to the universe.
— Nikola Tesla
Casting Out the Nines from PHI into Indigs reveals the Cosmic Harmonic Code.
— Junglelord.
Knowledge is Structured in Consciouness. Structure and Function Cannot Be Seperated.
— Junglelord

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Re: Plasma Aircraft/Spacecraft Technology

Post by junglelord » Mon Apr 07, 2008 8:14 am

Theoretical work with Sputnik

Due to the obvious military applications of the subject, there are few readily available experimental studies of plasma's effect on the radar cross section (RCS) of aircraft, but plasma interaction with microwaves is a well explored area of general plasma physics. Standard plasma physics reference texts are a good starting point and usually spend some time discussing wave propagation in plasmas.

One of the most interesting articles related to the effect of plasma on the RCS of aircraft was published in 1963 by the IEEE. The article is entitled "Radar cross sections of dielectric or plasma coated conducting spheres and circular cylinders" (IEEE Transactions on Antennas and Propagation, September 1963, pp. 558-569). Six years earlier—in 1957—the Soviets had launched the first artificial satellite. While trying to track Sputnik it was noticed that its electromagnetic scattering properties were different from what was expected for a conductive sphere. This was due to the satellite's traveling inside of a plasma shell: the ionosphere.

The Sputnik's simple shape serves as an ideal illustration of plasma's effect on the RCS of an aircraft. Naturally, an aircraft would have a far more elaborate shape and be made of a greater variety of materials, but the basic effect should remain the same. In the case of the Sputnik flying through the ionosphere at high velocity and surrounded by a naturally-occurring plasma shell, there are two separate radar reflections: the first from the conductive surface of the satellite itself and the second from the dielectric plasma shell.

The authors of the paper found that a dielectric (plasma) shell may either decrease or increase the echo area of the object. If either one of the two reflections is considerably greater, then the weaker reflection will not contribute much to the overall effect. The authors also stated that the EM signal that penetrates the plasma shell and reflects off the object's surface will drop in intensity while traveling through plasma, as was explained in the previous section.

The most interesting effect is observed when the two reflections are of the same order of magnitude. In this situation the two components (the two reflections) will be added as phasors and the resulting field will determine the overall RCS. When these two components are out of phase relative to each other, cancellation occurs. This means that under such circumstances the RCS becomes null and the object is completely invisible to the radar.

It is immediately apparent that performing similar numeric approximations for the complex shape of an aircraft would be difficult. This would require a large body of experimental data for the specific airframe, properties of plasma, aerodynamic aspects, incident radiation, etc. On the other hand, the original computations discussed in this paper were done by a handful of people on an IBM 704 computer made in 1956, and at the time, this was a novel subject with very little research background. So much has changed in science and engineering since 1963 that differences between a metal sphere and a modern combat jet pale in comparison.

A simple application of plasma stealth is the use of plasma as an antenna: metal antenna masts often have large radar cross sections, but a hollow glass tube filled with low pressure plasma can also be used as an antenna, and is entirely transparent to radar when not in use.

http://en.wikipedia.org/wiki/Plasma_stealth
If you only knew the magnificence of the 3, 6 and 9, then you would have a key to the universe.
— Nikola Tesla
Casting Out the Nines from PHI into Indigs reveals the Cosmic Harmonic Code.
— Junglelord.
Knowledge is Structured in Consciouness. Structure and Function Cannot Be Seperated.
— Junglelord

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Re: Plasma Aircraft/Spacecraft Technology

Post by junglelord » Thu Apr 17, 2008 7:52 am

Relativistic Birkeland Currents power the TR-3B

Belgium Flying Triangle (the real deal)
http://www.youtube.com/watch?v=qpGc8w5Wu0Y
Physics Analysis Of TR-3B
From FoucheMedia
FoucheMedia@satx.rr.com
11-9-00


Thought you might be interested in an article posted by John Kooiman about the TR-3B gravity warping technology. I will depend on my esteemed friends and colleges who actually understand physics to rebut or support his premise. Love to hear your thoughts. After the revelation about the USAF's saucer programs in the last few months, things are getting more interesting. Especially as I stated 3 years ago that we had researched, reverse engineered, and built many saucer type prototypes since the 50s.

Ed Fouche
Efouche@satx.rr.com
210 681-2595

_____

From John Kooiman
john.kooiman@home.com
TR-3B Antigravity Physics Explained

To be correct, I probably should say, "TR-3B Antigravity Physics Explained, insofar as General Relativity can be considered an explanation for gravity."


Many readers of this list are probably already familiar with Edgar Fouche's description of the USA's Top Secret TR-3B triangular shaped nuclear powered aerospace craft. If not, read about it here: http://fouchemedia.com/arap/speech.htm

Mr. Fouche describes the TR-3B's propulsion system as follows:

"A circular, plasma filled accelerator ring called the Magnetic Field Disrupter, surrounds the rotatable crew compartment and is far ahead of any imaginable technology... The plasma, mercury based, is pressurized at 250,000 atmospheres at a temperature of 150 degrees Kelvin, and accelerated to 50,000 rpm to create a super-conductive plasma with the resulting gravity disruption.

The MFD generates a magnetic vortex field, which disrupts or neutralizes the effects of gravity on mass within proximity, by 89 percent...

The current MFD in the TR-3B causes the effect of making the vehicle extremely light, and able to outperform and outmaneuver any craft yet ...My sources say the performance is limited only the stresses that the human pilots can endure. Which is a lot, really, considering along with the 89% reduction in mass, the G forces are also reduced by 89%.

The crew of the TR-3B should be able to comfortable take up to 40Gs... Reduced by 89%, the occupants would feel about 4.2 Gs.

The TR-3Bs propulsion is provided by 3 multimode thrusters mounted at each bottom corner of the triangular platform. The TR-3 is a sub-Mach 9 vehicle until it reaches altitudes above l20,000 feet - then who knows how fast it can go!..."


I was skeptical of Mr. Fouche's claims when I first read them, as I'm sure that many of you are, but I was interested enough to do further research on what happens when you spin a plasma at high speeds in a ring (toroidal) configuration. I came across a physics article (sorry, I can't seem to locate the source right now) that described this exact configuration. The article said that, surprisingly, the charged particles of the plasma don't just spin uniformly around the ring, but they tend to take up a synchronized, tightly pitched, helical (screw thread) motion as they move around the ring. This can be understood in a general way as follows: the charged particles moving around the ring act as a current that in turn sets up a magnetic field around the ring. It is a well-known fact that electrons (or ions) tend to move in a helical fashion around magnetic field lines. Although it is a highly complex interaction, it only requires a small leap of faith to believe that the end result of these interactions between the moving charged particles (current) and associated magnetic fields results in the helical motion described above. In other words, the charged particles end up moving in very much the same pattern as the current on a wire tightly wound around a toroidal core.

I thought that this was an interesting fact, but didn't see how it could possibly relate to antigravity, until I ran across the following article: "Guidelines to Antigravity" by Dr. Robert Forward, written in 1962 (available at: http://www.whidbey.com/forward/pdf/tp007.pdf). Dr. Forward's article describes several little known aspects of Einstein's General Relativity Theory that indicate how moving matter can create unusual gravitational effects. When I saw Figure 5 in Dr. Forward's article, the pieces of the puzzle all fell together. I instantly saw how the moving matter pattern that Dr. Forward describes as necessary to generate a gravitational dipole was exactly the same as the plasma ring pattern described in the physics article discussed above! If Fouche's description is even close to correct, then the TR-3B utilizes this little known loophole in General Relativity Theory to create it's antigravity effects! Even though the TR-3B can only supposedly cancel 89% of gravity (and inertia) today, there is no reason why the technology can't be improved to exceed 100% and achieve true antigravity capability!

In theory, this same moving matter pattern could be mechanically reproduced by mounting a bunch of small gyroscopes all around the larger ring, with their axis on the larger ring, and then spinning both the gyroscopes and the ring at high speeds. However, as Dr. Forward points out any such mechanical system would probably fly apart before any significant antigravity effects could be generated. However, as Dr. Forward states, "By using electromagnetic forces to contain rotating systems, it would be possible for the masses to reach relativistic velocities; thus a comparatively small amount of matter, if dense enough and moving fast enough, could produce usable gravitational effects."

The requirement for a dense material moving at relativistic speeds would explain the use of Mercury plasma (heavy ions). If the plasma really spins at 50,000 RPM and the Mercury ions are also moving in a tight pitched spiral, then the individual ions would be moving probably hundreds, perhaps thousands of times faster than the bulk plasma spin, in order to execute their "screw thread" motions. It is quite conceivable that the ions could be accelerated to relativistic speeds in this manner. I am guessing that you would probably want to strip the free electrons from the plasma, making a positively charged plasma, since the free electrons would tend to counter rotate and reduce the efficiency of the antigravity device.

One of Einstein's postulates of GR says that gravitational mass and inertial mass are equivalent. This is consistent with Mr. Fouche's claim that inertial mass within the plasma ring is also reduced by 89%. This would also explain why the vehicle is triangular shaped. Since it still requires conventional thrusters for propulsion, the thrusters would need to be located outside of the "mass reduction zone" or else the mass of the thruster's reaction material would also be reduced, making them terribly inefficient. Since it requires a minimum of 3 legs to have a stable stool, it follows that they would need a minimum of 3 thrusters to have a stable aerospace platform. Three thrusters, located outside of the plasma ring, plus appropriate structural support, would naturally lead to a triangular shape for the vehicle.

I was extremely skeptical of Mr. Fouche's claimed size for the TR-3B, of 600 feet across. At first, I thought that this must be a typo. Why would anyone in their right mind build a "Tactical Reconnaissance" vehicle 2 football fields long? They must be nuts! However, the answer to this may also be found in Dr. Forward's paper. As Dr. Forward's puts it, "...even the most optimistic calculations indicate that very large devices will be required to create usable gravitational forces. Antigravity...like all modern sciences, will require special projects involving large sums of money, men, and energy."


FYI: This article has been posted to KeelyNet. You have permission to post it on your Web site, as long as proper creditation is provided.


http://www.rense.com/general5/trb.htm
If you only knew the magnificence of the 3, 6 and 9, then you would have a key to the universe.
— Nikola Tesla
Casting Out the Nines from PHI into Indigs reveals the Cosmic Harmonic Code.
— Junglelord.
Knowledge is Structured in Consciouness. Structure and Function Cannot Be Seperated.
— Junglelord

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Re: Plasma Aircraft/Spacecraft Technology

Post by skyfish » Wed Mar 25, 2009 7:28 pm

This is entertaining:

http://www.stargate-chronicles.com/oniondrive/onion.htm
By the very laws of electromagnetism, once the vortex filament is generated it becomes extremely stable, because of it’s plasma’s associated magnetic fields and the pinch effect in those fields (much in the same way a tornado’s rotating electrically charged sheath becomes self-confining once it has been established).
Interesting combination of materials and concepts.
Again...plasma vortex....

skyfish

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