Method-Apparatus for Altering Earth’s Atmosphere, Ionosphere, Magnetosphere. Harp

Method-Apparatus for Altering Earth’s Atmosphere, Ionosphere, Magnetosphere. Harp


A method and apparatus for altering at least one selected region which normally
exists above the earth’s surface. The region is excited by electron cyclotron
resonance heating to thereby increase its charged particle density.

In one embodiment, circularly polarized electromagnetic radiation is transmitted upward in
a direction substantially parallel to and along a field line which extends through
the region of plasma to be altered.

The radiation is transmitted at a frequency which excites electron cyclotron resonance to heat and accelerate the charged particles.

This increase in energy can cause ionization of neutral particles which
are then absorbed as part of the region thereby increasing the charged particle
density of the region.

1. A method for altering at least one region normally existing above the earth’s
surface with electromagnetic radiation using naturally-occurring and diverging
magnetic field lines of the earth comprising transmitting first electromagnetic
radiation at a frequency between 20 and 7200 kHz from the earth’s surface, said
transmitting being conducted essentially at the outset of transmission
substantially parallel to and along at least one of said field lines, adjusting the
frequency of said first radiation to a value which will excite electron cyclotron
resonance at an initial elevation at least 50 km above the earth’s surface, whereby
in the region in which said electron cyclotron resonance takes place heating,
further ionization, and movement of both charged and neutral particles is effected,
said cyclotron resonance excitation of said region is continued until the electron
concentration of said region reaches a value of at least 10.sup.6 per cubic
centimeter and has an ion energy of at least 2 ev.
2. The method of claim 1 including the step of providing artificial particles in
said at least one region which are excited by said electron cyclotron resonance.
3. The method of claim 2 wherein said artificial particles are provided by
injecting same into said at least one region from an orbiting satellite.
4. The method of claim 1 wherein said threshold excitation of electron cyclotron
resonance is about 1 watt per cubic centimeter and is sufficient to cause movement
of a plasma region along said diverging magnetic field lines to an altitude higher
than the altitude at which said excitation was initiated.
5. The method of claim 4 wherein said rising plasma region pulls with it a
substantial portion of neutral particles of the atmosphere which exist in or near
said plasma region.
6. The method of claim 1 wherein there is provided at least one separate source of
second electromagnetic radiation, said second radiation having at least one
frequency different from said first radiation, impinging said at least one second
radiation on said region while said region is undergoing electron cyclotron
resonance excitation caused by said first radiation.
7. The method of claim 6 wherein said second radiation has a frequency which is
absorbed by said region.
8. The method of claim 6 wherein said region is plasma in the ionosphere and said
second radiation excites plasma waves within said ionosphere.
9. The method of claim 8 wherein said electron concentration reaches a value of at
least 10.sup.12 per cubic centimeter.
10. The method of claim 8 wherein said excitation of electron cyclotron resonance
is initially carried out within the ionosphere and is continued for a time
sufficient to allow said region to rise above said ionosphere.
11. The method of claim 1 wherein said excitation of electron cyclotron resonance
is carried out above about 500 kilometers and for a time of from 0.1 to 1200
seconds such that multiple heating of said plasma region is achieved by means of
stochastic heating in the magnetosphere.
12. The method of claim 1 wherein said first electromagnetic radiation is right
hand circularly polarized in the northern hemisphere and left hand circularly
polarized in the southern hemisphere.

13. The method of claim 1 wherein said electromagnetic radiation is generated at
the site of a naturally-occurring hydrocarbon fuel source, said fuel source being
located in at least one of northerly or southerly magnetic latitudes.
14. The method of claim 13 wherein said fuel source is natural gas and electricity
for generating said electromagnetic radiation is obtained by burning said natural
gas in at least one of magnetohydrodynamic, gas turbine, fuel cell, and EGD
electric generators located at the site where said natural gas naturally occurs in
the earth.
15. The method of claim 14 wherein said site of natural gas is within the magnetic
latitudes that encompass Alaska.

1. Technical Field
This invention relates to a method and apparatus for altering at least one selected
region normally existing above the earth’s surface and more particularly relates to
a method and apparatus for altering said at least one region by initially
transmitting electromagnetic radiation from the earth’s surface essentially
parallel to and along naturally-occurring, divergent magnetic field lines which
extend from the earth’s surface through the region or regions to be altered.
2. Background Art
In the late 1950’s, it was discovered that naturally-occuring belts exist at high
altitudes above the earth’s surface, and it is now established that these belts
result from charged electrons and ions becoming trapped along the magnetic lines of
force (field lines) of the earth’s essentially dipole magnetic field.

The trapped electrons and ions are confined along the field lines between two magnetic mirrors
which exist at spaced apart points along those field lines. The trapped electrons
and ions move in helical paths around their particular field lines and “bounce”
back and forth between the magnetic mirrors.

These trapped electrons and ions can oscillate along the field lines for long periods of time.
In the past several years, substantial effort has been made to understand and
explain the phenomena involved in belts of trapped electrons and ions, and to
explore possible ways to control and use these phenomena for beneficial purposes.
For example, in the late 1950’s and early 1960’s both the United States and
U.S.S.R. detonated a series of nuclear devices of various yields to generate large
numbers of charged particles at various altitudes, e.g., 200 kilometers (km) or

This was done in order to establish and study artifical belts of trapped
electrons and ions. These experiments established that at least some of the
extraneous electrons and ions from the detonated devices did become trapped along
field lines in the earth’s magnetosphere to form artificial belts which were stable
for prolonged periods of time.

For a discussion of these experiments see

“The Radiation Belt and Magnetosphere”, W. N. Hess, Blaisdell Publishing Co., 1968, pps.
155 et sec.
Other proposals which have been advanced for altering existing belts of trapped
electrons and ions and/or establishing similar artificial belts include injecting
charged particles from a satellite carrying a payload of radioactive beta-decay
material or alpha emitters; and injecting charged particles from a satellite-borne
electron accelerator.

Still another approach is described in U.S. Pat. No. 4,042,196 wherein a low energy ionized gas, e.g., hydrogen, is released from a synchronous orbiting satellite near the apex of a radiation belt which is
naturally-occurring in the earth’s magnetosphere to produce a substantial increase
in energetic particle precipitation and, under certain conditions, produce a limit
in the number of particles that can be stably trapped.

This precipitation effect arises from an enhancement of the whistler-mode and ion-cyclotron mode interactions that result from the ionized gas or “cold plasma” injection.

It has also been proposed to release large clouds of barium in the magnetosphere so
that photoionization will increase the cold plasma density, thereby producing
electron precipitation through enhanced whistler-mode interactions.

However, in all of the above-mentioned approaches, the mechanisms involved in
triggering the change in the trapped particle phenomena must be actually positioned
within the affected zone, e.g., the magnetosphere, before they can be actuated to
effect the desired change.

The earth’s ionosphere is not considered to be a “trapped” belt since there are few
trapped particles therein.

The term “trapped” herein refers to situations where the force of gravity on the                            trapped particles is balanced by magnetic forces rather than hydrostatic or collisional forces.

The charged electrons and ions in the ionosphere also follow helical paths around magnetic field lines within the ionosphere but are not trapped between mirrors, as in the case of the trapped belts
in the magnetosphere, since the gravitational force on the particles is balanced by
collisional or hydrostatic forces.

In recent years, a number of experiments have actually been carried out to modify
the ionosphere in some controlled manner to investigate the possibility of a
beneficial result.

For detailed discussions of these operations see the following papers:

(1) Ionospheric Modification Theory; G. Meltz and F. W. Perkins;

(2) The Platteville High Power Facility; Carrol et al.; (3) Arecibo Heating Experiments; W.
E. Gordon and H. C. Carlson, Jr.; and (4) Ionospheric Heating by Powerful Radio
Waves; Meltz et al., all published in Radio Science, Vol. 9, No. 11, November,
1974, at pages 885-888; 889-894; 1041-1047; and 1049-1063, respectively, all of
which are incorporated herein by reference.

In such experiments, certain regions of the ionosphere are heated to change the electron density and temperature within these regions.

This is accomplished by transmitting from earth-based antennae high
frequency electromagnetic radiation at a substantial angle to, not parallel to, the
ionosphere’s magnetic field to heat the ionospheric particles primarily by ohmic

The electron temperature of the ionosphere has been raised by hundreds of
degrees in these experiments, and electrons with several electron volts of energy
have been produced in numbers sufficient to enhance airglow.

Electron concentrations have been reduced by a few percent, due to expansion of the plasma
as a result of increased temperature.

In the Elmo Bumpy Torus (EBT), a controlled fusion device at the Oak Ridge National
Laboratory, all heating is provided by microwaves at the electron cyclotron
resonance interaction.

A ring of hot electrons is formed at the earth’s surface in the magnetic mirror by a combination of electron cyclotron resonance and stochastic heating.

In the EBT, the ring electrons are produced with an average “temperature”
of 250 kilo electron volts or kev (2.5.times.10.sup.9 K) and a plasma beta between
0.1 and 0.4; see,

“A Theoretical Study of Electron–Cyclotron Absorption in Elmo Bumpy Torus”, Batchelor and Goldfinger, Nuclear Fusion, Vol. 20, No. 4 (1980) pps. 403-418.

Electron cyclotron resonance heating has been used in experiments on the earth’s
surface to produce and accelerate plasmas in a diverging magnetic field. Kosmahl et
al. showed that power was transferred from the electromagnetic waves and that a
fully ionized plasma was accelerated with a divergence angle of roughly 13 degrees.
Optimum neutral gas density was 1.7.times.10.sup.14 per cubic centimeter;

“Plasma Acceleration with Microwaves Near Cyclotron Resonance”, Kosmahl et al.,



The present invention provides a method and apparatus for altering at least one
selected region which normally exists above the earth’s surface.

The region is excited by electron cyclotron resonance heating of electrons which are already
present and/or artifically created in the region to thereby increase the charged
particle energy and ultimately the density of the region.

In one embodiment this is done by transmitting circularly polarized electromagnetic
radiation from the earth’s surface at or near the location where a naturallyoccurring
dipole magnetic field (force) line intersects the earth’s surface.

Right hand circular polarization is used in the northern hemisphere and left hand
circular polarization is used in the southern hemisphere.

The radiation is deliberately transmitted at the outset in a direction substantially parallel to and
along a field line which extends upwardly through the region to be altered.

The radiation is transmitted at a frequency which is based on the gyrofrequency of the
charged particles and which, when applied to the at least one region, excites
electron cyclotron resonance within the region or regions to heat and accelerate
the charged particles in their respective helical paths around and along the field

Sufficient energy is employed to cause ionization of neutral particles
(molecules of oxygen, nitrogen and the like, particulates, etc.) which then become
a part of the region thereby increasing the charged particle density of the region.
This effect can further be enhanced by providing artificial particles, e.g.,
electrons, ions, etc., directly into the region to be affected from a rocket,
satellite, or the like to supplement the particles in the naturally-occurring

These artificial particles are also ionized by the transmitted
electromagnetic radiation thereby increasing charged particle density of the
resulting plasma in the region.

In another embodiment of the invention, electron cyclotron resonance heating is
carried out in the selected region or regions at sufficient power levels to allow a
plasma present in the region to generate a mirror force which forces the charged
electrons of the altered plasma upward along the force line to an altitude which is
higher than the original altitude.

In this case the relevant mirror points are at the base of the altered region or regions. The charged electrons drag ions with them as well as other particles that may be present. Sufficient power, e.g.,
10.sup.15 joules, can be applied so that the altered plasma can be trapped on the
field line between mirror points and will oscillate in space for prolonged periods
of time.

By this embodiment, a plume of altered plasma can be established at
selected locations for communication modification or other purposes.
In another embodiment, this invention is used to alter at least one selected region
of plasma in the ionosphere to establish a defined layer of plasma having an
increased charged particle density.

Once this layer is established, and while maintaining the transmission of the main beam of circularly polarized electromagnetic radiation, the main beam is modulated and/or at least one second different, modulated electromagnetic radiation beam is transmitted from at least
one separate source at a different frequency which will be absorbed in the plasma

The amplitude of the frequency of the main beam and/or the second beam or
beams is modulated in resonance with at least one known oscillation mode in the
selected region or regions to excite the known oscillation mode to propagate a
known frequency wave or waves throughout the ionosphere.


The actual construction, operation, and apparent advantages of this invention will
be better understood by referring to the drawings in which like numerals identify
like parts and in which:

U.S. Patent No. 4,686,605
FIG. 1 is a simplified schematical view of the earth (not to scale) with a magnetic
field (force) line along which the present invention is carried out;

FIG. 2 is one embodiment within the present invention in which a selected region of
plasma is raised to a higher altitude;

FIG. 3 is a simplified, idealized representation of a physical phenomenon involved
in the present invention;

FIG. 4 is a schematic view of another embodiment within the present invention.

FIG. 5 is a schematic view of an apparatus embodiment within this invention .


The earth’s magnetic field is somewhat analogous to a dipole bar magnet. As such,
the earth’s magnetic field contains numerous divergent field or force lines, each
line intersecting the earth’s surface at points on opposite sides of the Equator.

The field lines which intersect the earth’s surface near the poles have apexes
which lie at the furthest points in the earth’s magnetosphere while those closest
to the Equator have apexes which reach only the lower portion of the magnetosphere.

At various altitudes above the earth’s surface, e.g., in both the ionosphere and
the magnetosphere, plasma is naturally present along these field lines. This plasma
consists of equal numbers of positively and negatively charged particles (i.e.,
electrons and ions) which are guided by the field line. It is well established that
a charged particle in a magnetic field gyrates about field lines, the center of
gyration at any instance being called the “guiding center” of the particle.

As the gyrating particle moves along a field line in a uniform field, it will follow a
helical path about its guiding center, hence linear motion, and will remain on the
field line.

Electrons and ions both follow helical paths around a field line but
rotate in opposite directions.

The frequencies at which the electrons and ions rotate about the field line are called gyromagnetic frequencies or cyclotron frequencies because they are identical with the expression for the angular
frequencies of gyration of particles in a cyclotron. The cyclotron frequency of
ions in a given magnetic field is less than that of electrons, in inverse proportion to their masses.

If the particles which form the plasma along the earth’s field lines continued to
move with a constant pitch angle, often designated “alpha”, they would soon impact
on the earth’s surface. Pitch angle alpha is defined as the angle between the
direction of the earth’s magnetic field and the velocity (V) of the particle.

However, in converging force fields, the pitch angle does change in such a way as
to allow the particle to turn around and avoid impact. Consider a particle moving
along a field line down toward the earth.

It moves into a region of increasing magnetic field strength and therefore sine alpha increases. But sine alpha can only increase to 1.0, at which point, the particle turns around and starts moving up
along the field line, and alpha decreases.

The point at which the particle turns around is called the mirror point, and there alpha equals ninety degrees.

This process is repeated at the other end of the field line where the same magnetic
field strength value B, namely Bm, exists. The particle again turns around and this
is called the “conjugate point” of the original mirror point.

The particle is therefore trapped and bounces between the two magnetic mirrors. The particle can
continue oscillating in space in this manner for long periods of time.

The actual place where a particle will mirror can be calculated from the following:

sin.sup.2 alpha.sub.o =B.sub.o /B.sub.m

(1) wherein:

U.S. Patent No. 4,686,605 alpha.sub.o =equatorial pitch angle of particle
B.sub.o =equatorial field strength on a particular field line
B.sub.m =field strength at the mirror point

Recent discoveries have established that there are substantial regions of naturally
trapped particles in space which are commonly called “trapped radiation belts”.
These belts occur at altitudes greater than about 500 km and accordingly lie in the
magnetosphere and mostly above the ionosphere.

The ionosphere, while it may overlap some of the trapped-particle belts, is a
region in which hydrostatic forces govern its particle distribution in the
gravitational field. Particle motion within the ionosphere is governed by both
hydrodynamic and electrodynamic forces.

While there are few trapped particles in the ionosphere, nevertheless, plasma is present along field lines in the ionosphere.

The charged particles which form this plasma move between collisions
with other particles along similar helical paths around the field lines and
although a particular particle may diffuse downward into the earth’s lower
atmosphere or lose energy and diverge from its original field line due to
collisions with other particles, these charged particles are normally replaced by
other available charged particles or by particles that are ionized by collision
with said particle.

The electron density (N.sub.e) of the plasma will vary with the
actual conditions and locations involved. Also, neutral particles, ions, and
electrons are present in proximity to the field lines.

The production of enhanced ionization will also alter the distribution of atomic
and molecular constituents of the atmosphere, most notably through increased atomic
nitrogen concentration.

The upper atmosphere is normally rich in atomic oxygen (the
dominant atmospheric constituent above 200 km altitude), but atomic nitrogen is
normally relatively rare. This can be expected to manifest itself in increased
airglow, among other effects.

As known in plasma physics, the characteristics of a plasma can be altered by
adding energy to the charged particles or by ionizing or exciting additional
particles to increase the density of the plasma.

One way to do this is by heating the plasma which can be accomplished in different ways, e.g., ohmic, magnetic compression, shock waves, magnetic pumping, electron cyclotron resonance, and the like.

Since electron cyclotron resonance heating is involved in the present invention, a
brief discussion of same is in order.

Increasing the energy of electrons in a plasma by invoking electron cyclotron resonance heating, is based on a principle similar to that utilized to accelerate charged particles in a cyclotron.

If a plasma is confined by a static axial magnetic field of strength B, the charged
particles will gyrate about the lines of force with a frequency given, in hertz, as
f.sub.g =1.54.times.10.sup.3 B/A, where: B=magnetic field strength in gauss, and
A=mass number of the ion.

Suppose a time-varying field of this frequency is superimposed on the static field
B confining the plasma, by passage of a radiofrequency current through a coil which
is concentric with that producing the axial field, then in each half-cycle of their
rotation about the field lines, the charged particles acquire energy from the
oscillating electric field associated with the radio frequency.

For example, if B is 10,000 gauss, the frequency of the field which is in resonance with protons in a
plasma is 15.4 megahertz.

As applied to electrons, electron cyclotron resonance heating requires an
oscillating field having a definite frequency determined by the strength of the confining field.

The radio-frequency radiation produces time-varying fields
(electric and magnetic), and the electric field accelerates the charged particle.

The energized electrons share their energy with ions and neutrals by undergoing
collisions with these particles, thereby effectively raising the temperature of the
electrons, ions, and neutrals.

The apportionment of energy among these species is determined by collision frequencies.

For a more detailed understanding of the physics involved, see “Controlled Thermonuclear Reactions”, Glasstone and Lovberg, D. Van Nostrand Company, Inc., Princeton, N.J., 1960 and

“The Radiation Belt and Magnetosphere”, Hess, Blaisdell Publishing Company, 1968, both of which are incorporated herein by reference.

Referring now to the drawings, the present invention provides a method and
apparatus for altering at least one region of plasma which lies along a field line,
particularly when it passes through the ionosphere and/or magnetosphere.

FIG. 1 is a simplified illustration of the earth 10 and one of its dipole magnetic force or
field lines 11.

As will be understood, line 11 may be any one of the numerous
naturally existing field lines and the actual geographical locations 13 and 14 of
line 11 will be chosen based on a particular operation to be carried out.

The actual locations at which field lines intersect the earth’s surface is documented
and is readily ascertainable by those skilled in the art.

Line 11 passes through region R which lies at an altitude above the earth’s

A wide range of altitudes are useful given the power that can be employed
by the practice of this invention.

The electron cyclotron resonance heating effect can be made to act on electrons anywhere above the surface of the earth.

These electrons may be already present in the atmosphere, ionosphere, and/or
magnetosphere of the earth, or can be artificially generated by a variety of means
such as x-ray beams, charged particle beams, lasers, the plasma sheath surrounding
an object such as a missile or meteor, and the like.

Further, artificial particles, e.g., electrons, ions, etc., can be injected directly into region R from an earthlaunched rocket or orbiting satellite carrying, for example, a payload of
radioactive beta-decay material; alpha emitters; an electron accelerator; and/or
ionized gases such as hydrogen; see U.S. Pat. No. 4,042,196.

The altitude can be greater than about 50 km if desired, e.g., can be from about 50 km to about 800 km, and, accordingly may lie in either the ionosphere or the magnetosphere or both.

As explained above, plasma will be present along line 11 within region R and is
represented by the helical line 12. Plasma 12 is comprised of charged particles
(i.e., electrons and ions) which rotate about opposing helical paths along line 11.

Antenna 15 is positioned as close as is practical to the location 14 where line 11
intersects the earth’s surface. Antenna 15 may be of any known construction for
high directionality, for example, a phased array, beam spread angle (.theta.) type.
See “The MST Radar at Poker Flat, Alaska”, Radio Science, Vol. 15, No. 2, Mar.-Apr.
1980, pps. 213-223, which is incorporated herein by reference.

Antenna 15 is coupled to transmitter 16 which generates a beam of high frequency electromagnetic
radiation at a wide range of discrete frequencies, e.g., from about 20 to about
1800 kilohertz (kHz).

Transmitter 16 is powered by power generator means 17 which is preferably comprised
of one or more large, commercial electrical generators.

Some embodiments of the present invention require large amounts of power, e.g., up to 10.sup.9 to 10.sup.11 watts, in continuous wave or pulsed power.

Generation of the needed power is within the state of the art. Although the electrical generators necessary for the practice of the invention can be powered in any known manner, for example, by nuclear reactors, hydroelectric facilities, hydrocarbon fuels, and the like, this
invention, because of its very large power requirement in certain applications, is
particularly adapted for use with certain types of fuel sources which naturally
occur at strategic geographical locations around the earth.

For example, large reserves of hydrocarbons (oil and natural gas) exist in Alaska and Canada. In
northern Alaska, particularly the North Slope region, large reserves are currently                         readily available.

Alaska and northern Canada also are ideally located geographically as to magnetic latitudes. Alaska provides easy access to magnetic field lines that are especially suited to the practice of this invention, since many field lines which extend to desirable altitudes for this invention intersect
the earth in Alaska.

Thus, in Alaska, there is a unique combination of large,
accessible fuel sources at desirable field line intersections.

Further, a particularly desirable fuel source for the generation of very large amounts of
electricity is present in Alaska in abundance, this source being natural gas.

The presence of very large amounts of clean-burning natural gas in Alaskan latitudes,
particularly on the North Slope, and the availability of magnetohydrodynamic (MHD),
gas turbine, fuel cell, electrogasdynamic (EGD) electric generators which operate
very efficiently with natural gas provide an ideal power source for the
unprecedented power requirements of certain of the applications of this invention.

For a more detailed discussion of the various means for generating electricity from
hydrocarbon fuels, see “Electrical Aspects of Combustion”, Lawton and Weinberg,
Clarendon Press, 1969.

For example, it is possible to generate the electricity directly at the high frequency needed to drive the antenna system.

To do this, typically the velocity of flow of the combustion gases (v), past magnetic field
perturbation of dimension d (in the case of MHD), follow the rule:
v=df where f is the frequency at which electricity is generated.

Thus, if v=1.78.times.10.sup.6 cm/sec and d=1 cm then electricity would be generated at a
frequency of 1.78 mHz.

Put another way, in Alaska, the right type of fuel (natural gas) is naturally
present in large amounts and at just the right magnetic latitudes for the most
efficient practice of this invention, a truly unique combination of circumstances.

Desirable magnetic latitudes for the practice of this invention interest the
earth’s surface both northerly and southerly of the equator, particularly desirable
latitudes being those, both northerly and southerly, which correspond in magnitude
with the magnetic latitudes that encompass Alaska.

Referring now to FIG. 2 a first ambodiment is illustrated where a selected region
R.sub.1 of plasma 12 is altered by electron cyclotron resonance heating to
accelerate the electrons of plasma 12, which are following helical paths along
field line 11.

To accomplish this result, electromagnetic radiation is transmitted at the outset,
essentially parallel to line 11 via antenna 15 as right hand circularly polarized
radiation wave 20.

Wave 20 has a frequency which will excite electron cyclotron resonance with plasma 12 at its initial or original altitude. This frequency will vary depending on the electron cyclotron resonance of region R.sub.1 which, in turn, can be determined from available data based on the altitudes of region R.sub.1, the particular field line 11 being used, the strength of the earth’s
magnetic field, etc. Frequencies of from about 20 to about 7200 kHz, preferably
from about 20 to about 1800 kHz can be employed.

Also, for any given application, there will be a threshhold (minimum power level) which is needed to produce the desired result.

The minimum power level is a function of the level of plasma production and movement required, taking into consideration any loss processes that may be dominant in a particular plasma or propagation path.

As electron cyclotron resonance is established in plasma 12, energy is transferred
from the electromagnetic radiation 20 into plasma 12 to heat and accelerate the
electrons therein and, subsequently, ions and neutral particles.

As this process continues, neutral particles which are present within R.sub.1 are ionized and
absorbed into plasma 12 and this increases the electron and ion densities of plasma

As the electron energy is raised to values of about 1 kilo electron volt (kev),
the generated mirror force (explained below) will direct the excited plasma 12 upward                   along line 11 to form a plume R.sub.2 at an altitude higher than that of

Plasma acceleration results from the force on an electron produced by a nonuniform
static magnetic field (B).

The force, called the mirror force, is given by (2) where .mu. is the electron magnetic moment and .gradient. B is the gradient of themagnetic field, .mu. being further defined as:  W.sub..perp. /B=mV.sub..perp..sup.2 /2B
where W.sub..perp. is the kinetic energy in the direction perpendicular to that of
the magnetic field lines and B is the magnetic field strength at the line of force
on which the guiding center of the particle is located.

The force as represented by equation (2) is the force which is responsible for a particle obeying equation (1).

Since the magnetic field is divergent in region R.sub.1, it can be shown that the
plasma will move upwardly from the heating region as shown in FIG. 1 and further it
can be shown that 1/2M.sub.e V.sub.e.perp..sup.2 (x).apprxeq.1/2M.sub.e V.sub.e.perp..sup.2 (Y)
+1/2M.sub.i V.sub.i.parallel..sup.2 (Y)

(3)b where the left hand side is the initial electron transverse kinetic energy; the
first term on the right is the transverse electron kinetic energy at some point (Y)
in the expanded field region, while the final term is the ion kinetic energy
parallel to B at point (Y).

This last term is what constitutes the desired ion

It is produced by an electrostatic field set up by electrons which are
accelerated according to Equation (2) in the divergent field region and pulls ions
along with them. Equation (3) ignores electron kinetic energy parallel to B because
V.sub.e.parallel. .apprxeq.V.sub.i.parallel., so the bulk of parallel kinetic
energy resides in the ions because of their greater masses.

For example, if anelectromagnetic energy flux of from about 1 to about 10 watts per square centimeter is applied to region R, whose altitude is 115 km, a plasma having a density
(N.sub.e) of 10.sup.12 per cubic centimeter will be generated and moved upward to
region R.sub.2 which has an altitude of about 1000 km.

The movement of electrons in the plasma is due to the mirror force while the ions are moved by ambipolar diffusion (which results from the electrostatic field).

This effectively “lifts” a layer of plasma 12 from the ionosphere and/or magnetosphere to a higher elevation R.sub.2.

The total energy required to create a plasma with a base area of 3 square
kilometers and a height of 1000 km is about 3.times.10.sup.13 joules.

FIG. 3 is an idealized representation of movement of plasma 12 upon excitation by
electron cyclotron resonance within the earth’s divergent force field.

Electrons (e) are accelerated to velocities required to generate the necessary mirror force
to cause their upward movement.

At the same time neutral particles (n) which are present along line 11 in region R.sub.1 are ionized and become part of plasma 12.

As electrons (e) move upward along line 11, they drag ions (i) and neutrals (n)
with them but at an angle .theta. of about 13 degrees to field line 11.

Also, any particulates that may be present in region R.sub.1, will be swept upwardly with the

As the charged particles of plasma 12 move upward, other particles such as
neutrals within or below R.sub.1, move in to replace the upwardly moving particles.

These neutrals, under some conditions, can drag with them charged particles.
For example, as a plasma moves upward, other particles at the same altitude as the
plasma move horizontally into the region to replace the rising plasma and to form
new plasma.

The kinetic energy developed by said other particles as they move
horizontally is, for example, on the same order of magnitude as the total zonal

kinetic energy of stratospheric winds known to exist.
Referring again to FIG. 2, plasma 12 in region R.sub.1 is moved upward along field
line 11.

The plasma 12 will then form a plume (cross-hatched area in FIG. 2) which
will be relatively stable for prolonged periods of time.

The exact period of time will vary widely and be determined by gravitational forces and a combination of radiative and diffusive loss terms.

In the previous detailed example, the calculations were based on forming a plume by producing 0.sup.+ energies of 2 ev/particle. About 10 ev per particle would be required to expand plasma 12 to apex point C (FIG. 1).

There at least some of the particles of plasma 12 will be trapped
and will oscillate between mirror points along field line 11.

This oscillation will then allow additional heating of the trapped plasma 12 by stochastic heating which is associated with trapped and oscillating particles.

See “A New Mechanism for Accelerating Electrons in the Outer Ionosphere” by R. A. Helliwell and T. F. Bell, Journal of Geophysical Research, Vol. 65, No. 6, June, 1960.

This is preferably carried out at an altitude of at least 500 km.
The plasma of the typical example might be employed to modify or disrupt microwave
transmissions of satellites.

If less than total black-out of transmission is desired (e.g., scrambling by phase shifting digital signals), the density of the plasma (N.sub.e) need only be at least about 10.sup.6 per cubic centimeter for a plasma orginating at an altitude of from about 250 to about 400 km and accordingly less energy (i.e., electromagnetic radiation), e.g., 10.sup.8 joules need be

Likewise, if the density N.sub.e is on the order of 10.sup.8, a properly
positioned plume will provide a reflecting surface for VHF waves and can be used to
enhance, interfere with, or otherwise modify communication transmissions.

It can be seen from the foregoing that by appropriate application of various aspects of this
invention at strategic locations and with adequate power sources, a means and
method is provided to cause interference with or even total disruption of
communications over a very large portion of the earth.

This invention could be employed to disrupt not only land based communications, both civilian and military, but also airborne communications and sea communications (both surface and

This would have significant military implications, particularly as a
barrier to or confusing factor for hostile missiles or airplanes.

The belt or belts of enhanced ionization produced by the method and apparatus of this invention,
particularly if set up over Northern Alaska and Canada, could be employed as an
early warning device, as well as a communications disruption medium.

Further, the simple ability to produce such a situation in a practical time period can by itself
be a deterring force to hostile action.

The ideal combination of suitable field lines intersecting the earth’s surface at the point where substantial fuel sources are available for generation of very large quantitities of electromagnetic power, such as the North Slope of Alaska, provides the wherewithal to accomplish the
foregoing in a practical time period, e.g., strategic requirements could
necessitate achieving the desired altered regions in time periods of two minutes or
less and this is achievable with this invention, especially when the combination of
natural gas and magnetohydrodynamic, gas turbine, fuel cell and/or EGD electric
generators are employed at the point where the useful field lines intersect the
earth’s surface.

One feature of this invention which satisfies a basic requirement
of a weapon system, i.e., continuous checking of operability, is that small amounts
of power can be generated for operability checking purposes.

Further, in the exploitation of this invention, since the main electromagnetic beam which generates
the enhanced ionized belt of this invention can be modulated itself and/or one or
more additional electromagnetic radiation waves can be impinged on the ionized
region formed by this invention as will be described in greater detail herein after
with respect to FIG. 4, a substantial amount of randomly modulated signals of very
large power magnitude can be generated in a highly nonlinear mode.

This can cause confusion of or interference with or even complete disruption of guidance systems
employed by even the most sophisticated of airplanes and missiles.

The ability to employ and transmit over very wide areas of the earth a plurality of
electromagnetic waves of varying frequencies and to change same at will in a random                               manner, provides a unique ability to interfere with all modes of communications,
land, sea, and/or air, at the same time.

Because of the unique juxtaposition of usable fuel source at the point where desirable field lines intersect the earth’s surface, such wide ranging and complete communication interference can be achieved in a resonably short period of time.

Because of the mirroring phenomenon discussed herein above, it can also be prolonged for substantial time periods so that it would not be a mere transient effect that could simply be waited out by an opposing force.

Thus, this invention provides the ability to put unprecedented amounts of
power in the earth’s atmosphere at strategic locations and to maintain the power
injection level, particularly if random pulsing is employed, in a manner far more
precise and better controlled than heretofore accomplished by the prior art,
particularly by the detonation of nuclear devices of various yeilds at various

Where the prior art approaches yielded merely transitory effects, the
unique combination of fuel and desirable field lines at the point where the fuel
occurs allows the establishment of, compared to prior art approaches, precisely
controlled and long-lasting effects which cannot, practically speaking, simply be
waited out.

Further, by knowing the frequencies of the various electromagnetic
beams employed in the practice of this invention, it is possible not only to
interfere with third party communications but to take advantage of one or more such
beams to carry out a communications network even though the rest of the world’s
communications are disrupted.

Put another way, what is used to disrupt another’s communications can be employed by one knowledgeable of this invention as a communications network at the same time. In addition, once one’s own communication network is established, the far-reaching extent of the effects of this invention could be employed to pick up communication signals of other for intelligence

Thus, it can be seen that the disrupting effects achievable by this
invention can be employed to benefit by the party who is practicing this invention
since knowledge of the various electromagnetic waves being employed and how they
will vary in frequency and magnitude can be used to an advantage for positive
communication and eavesdropping purposes at the same time.

However, this invention is not limited to locations where the fuel source naturally exists or where
desirable field lines naturally intersect the earth’s surface.

For example, fuel, particularly hydrocarbon fuel, can be transported by pipeline and the like to the
location where the invention is to be practiced.
FIG. 4 illustrates another embodiment wherein a selected region of plasma R.sub.3
which lies within the earth’s ionosphere is altered to increase the density thereof
whereby a relatively stable layer 30 of relatively dense plasma is maintained
within region R.sub.3.

Electromagnetic radiation is transmitted at the outset essentially parallel to field line 11 via antenna 15 as a right hand circularly polarized wave and at a frequency (e.g., 1.78 megahertz when the magnetic field at the desired altitude is 0.66 gauss) capable of exciting electron cyclotron
resonance in plasma 12 at the particular altitude of plasma 12.

This causes heating of the particles (electrons, ions, neutrals, and particulates) and ionization of
the uncharged particles adjacent line 11, all of which are absorbed into plasma 12
to increase the density thereof.

The power transmitted, e.g., 2.times.10.sup.6 watts for up to 2 minutes heating time, is less than that required to generate the mirror force F required to move plasma 12 upward as in the previous embodiment.
While continuing to transmit electromagnetic radiation 20 from antenna 15, a second
electromagnetic radiation beam 31, which is at a defined frequency different from
the radiation from antenna 15, is transmitted from one or more second sources via
antenna 32 into layer 30 and is absorbed into a portion of layer 30 (cross-hatched
area in FIG. 4).

The electromagnetic radiation wave from antenna 32 is amplitude
modulated to match a known mode of oscillation f.sub.3 in layer 30.

This creates a resonance in layer 30 which excites a new plasma wave 33 which also has a frequency
of f.sub.3 and which then propogates through the ionosphere.

Wave 33 can be used to improve or disrupt communications or both depending on what is desired in a particular application. Of course, more than one new wave 33 can be generated and
the various new waves can be modulated at will and in a highly nonlinear fashion.

FIG. 5 shows apparatus useful in this invention, particularly when those
applications of this invention are employed which require extremely large amounts
of power.

In FIG. 5 there is shown the earth’s surface 40 with a well 41 extending
downwardly thereinto until it penetrates hydrocarbon producing reservoir 42.
Hydrocarbon reservoir 42 produces natural gas alone or in combination with crude

Hydrocarbons are produced from reservoir 42 through well 41 and wellhead 43 to
a treating system 44 by way of pipe 45. In treater 44, desirable liquids such as
crude oil and gas condensates are separated and recovered by way of pipe 46 while
undesirable gases and liquids such as water, H.sub.2 S, and the like are separated
by way of pipe 47.

Desirable gases such as carbon dioxide are separated by way of
pipe 48, and the remaining natural gas stream is removed from treater 44 by way of
pipe 49 for storage in conventional tankage means (not shown) for future use and/or
use in an electrical generator such as a magnetohydrodynamic, gas turbine, fuel
cell or EGD generator 50.

Any desired number and combination of different types of electric generators can be employed in the practice of this invention.

The natural gas is burned in generator 50 to produce substantial quantities of electricity
which is then stored and/or passed by way of wire 51 to a transmitter 52 which
generates the electromagnetic radiation to be used in the method of this invention.
The electromagnetic radiation is then passed by way of wire 53 to antenna 54 which
is located at or near the end of field line 11.

Antenna 54 sends circularly polarized radiation wave 20 upwards along field line 11 to carry out the various methods of this invention as described hereinabove.
Of course, the fuel source need not be used in its naturally-occurring state but
could first be converted to another second energy source form such as hydrogen,
hydrazine and the like, and electricity then generated from said second energy
source form.
It can be seen from the foregoing that when desirable field line 11 intersects
earth’s surface 40 at or near a large naturally-occurring hydrocarbon source 42,
exceedingly large amounts of power can be very efficiently produced and transmitted
in the direction of field lines.

This is particularly so when the fuel source is natural gas and magneto hydrodynamic generators are employed. Further, this can all be accomplished in a relatively small physical area when there is the unique coincidence of fuel source 42 and desirable field line 11.

Of course, only one set of equipment is shown in FIG. 5 for sake of simplicity. For a large hydrocarbon reservoir 42, a plurality of wells 41 can be employed to feed one or more storage
means and/or treaters and as large a number of generators 55 as needed to power one
or more transmitters 52 and one or more antennas 54.

Since all of the apparatus 44 through 54 can be employed and used essentially at the sight where naturallyoccurring fuel source 42 is located, all the necessary electromagnetic radiation 20
is generated essentially at the same location as fuel source 42.

This provides for a maximum amount of usable electromagnetic radiation 20 since there are no
significant storage or transportation losses to be incurred. In other words, the
apparatus is brought to the sight of the fuel source where desirable field line 11
intersects the earth’s surface 40 on or near the geographical location of fuel
source 42, fuel source 42 being at a desirable magnetic latitude for the practice
of this invention, for example, Alaska.
The generation of electricity by motion of a conducting fluid through a magnetic
field, i.e., magnetohydrodynamics (MHD), provides a method of electric power
generation without moving mechanical parts and when the conducting fluid is a
plasma formed by combustion of a fuel such as natural gas, an idealized combination
of apparatus is realized since the very clean-burning natural gas forms the
conducting plasma in an efficient manner and the thus formed plasma, when passed
through a magnetic field, generates electricity in a very efficient manner.

Thus, the use of fuel source 42 to generate a plasma by combustion thereof for the
generation of electricity essentially at the site of occurrence of the fuel source
is unique and ideal when high power levels are required and desirable field lines 11 intersect the earth’s surface 40 at or near the site of fuel source 42.

particular advantage for MHD generators is that they can be made to generate large
amounts of power with a small volume, light weight device. For example, a 1000
megawatt MHD generator can be construed using superconducting magnets to weigh
roughly 42,000 pounds and can be readily air lifted.
This invention has a phenomenal variety of possible ramifications and potential
future developments. As alluded to earlier, missile or aircraft destruction,
deflection, or confusion could result, particularly when relativistic particles are

Also, large regions of the atmosphere could be lifted to an unexpectedly
high altitude so that missiles encounter unexpected and unplanned drag forces with
resultant destruction or deflection of same.

Weather modification is possible by, for example, altering upper atmosphere wind patterns or altering solar absorption patterns by constructing one or more plumes of atmospheric particles which will act as a lens or focusing device.

Also as alluded to earlier, molecular modifications of the atmosphere can take place so that positive environmental effects can be achieved. Besides actually changing the molecular composition of an atmospheric region, a particular molecule or molecules can be chosen for increased presence.
For example, ozone, nitrogen, etc. concentrations in the atmosphere could be
artificially increased. Similarly, environmental enhancement could be achieved by
causing the breakup of various chemical entities such as carbon dioxide, carbon
monoxide, nitrous oxides, and the like.

Transportation of entities can also be realized when advantage is taken of the drag effects caused by regions of the atmosphere moving up along diverging field lines.

Small micron sized particles can be then transported, and, under certain circumstances and with the availability of sufficient energy, larger particles or objects could be similarly affected.
Particles with desired characteristics such as tackiness, reflectivity,
absorptivity, etc., can be transported for specific purposes or effects.

For example, a plume of tacky particles could be established to increase the drag on a
missile or satellite passing therethrough.

Even plumes of plasma having substantially less charged particle density than described above will produce drag effects on missiles which will affect a lightweight (dummy) missile in a manner
substantially different than a heavy (live) missile and this affect can be used to
distinguish between the two types of missiles.

A moving plume could also serve as a means for supplying a space station or for focusing vast amount of sunlight on selected portions of the earth. Surveys of global scope could also be realized
because the earth’s natural magnetic field could be significantly altered in a
controlled manner by plasma beta effects resulting in, for example, improved
magnetotelluric surveys.

Electromagnetic pulse defenses are also possible. The
earth’s magnetic field could be decreased or disrupted at appropriate altitudes to
modify or eliminate the magnetic field in high Compton electron generation (e.g.,
from high altitude nuclear bursts) regions.

High intensity, well controlled electrical fields can be provided in selected locations for various purposes.

For example, the plasma sheath surrounding a missile or satellite could be used as a
trigger for activating such a high intensity field to destroy the missile or
satellite. Further, irregularities can be created in the ionosphere which will
interfere with the normal operation of various types of radar, e.g., synthetic
aperture radar.

The present invention can also be used to create artificial belts
of trapped particles which in turn can be studied to determine the stability of
such parties.

Still further, plumes in accordance with the present invention can be
formed to simulate and/or perform the same functions as performed by the detonation
of a “heave” type nuclear device without actually having to detonate such a device

Thus it can be seen that the ramifications are numerous, far-reaching, and
exceedingly varied in usefulness.







Inventors: Eastlund; Bernard J. (Spring, TX)
Assignee: APTI, Inc. (Los Angeles, CA)
Appl. No.: 690333
Filed: January 10, 1985
Current U.S. Class: 361/231; 89/1.11; 244/158R; 380/59
Intern’l Class: H05B 006/64; H05C 003/00; H05H 001/46
Field of Search: 361/230,231 244/158 R 376/100 89/1.11 380/59

References Cited [Referenced By]
Other References
Liberty Magazine, (2/35) p. 7 N. Tesla.
New York Times (9/22/40) Section 2, p. 7 W. L. Laurence.
New York Times (12/8/15) p. 8 Col. 3.
Primary Examiner: Cangialosi; Salvatore
Attorney, Agent or Firm: MacDonald; Roderick W.

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