 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.
Atmospheric
Geoengineering is occuring in our skies daily, and on a worldwide
basis.
For those who doubt
the feasibility of these special operations, just take a look at the
following Patents.
Chemtrail Patents:
Method and apparatus for altering a region in the earth's atmosphere,
ionosphere, and/or magnetosphere
United States Patent 4,686,605 / Eastlund / August 11, 1987
http://164.195.100.11
Method
of modifying weather
United States Patent 6,315,213 / Cordani / November 13, 2001
http://164.195.100.11/
A method for
artificially modifying the weather by seeding rain clouds of a storm
with suitable cross-linked aqueous polymer. The polymer is dispersed
into the cloud and the wind of the storm agitates the mixture
causing the polymer to absorb the rain. This reaction forms a
gelatinous substance which precipitate to the surface below. Thus,
diminishing the clouds ability to rain.
Process for
absorbing ultraviolet radiation using dispersed melanin
United States Patent / 5,286,979 / Berliner / February 15, 1994
http://164.195.100.11/
This invention is a
process for absorbing ultraviolet radiation in the atmosphere by
dispersing melanin, its analogs, or derivatives into the atmosphere.
By appropriate choice of melanin composition, size of melanin
dispersoids, and their concentration, the melanin will absorb some
quantity of ultraviolet radiation and thereby lessen its overall
effect on the critters who would normally absorb such radiation.
Liquid
atomizing apparatus for aerial spraying
United States Patent / 4,948,050 / Picot / August 14, 1990
http://patft.uspto.gov/
A rotary liquid
spray atomizer for aerial spraying is driven by a variable speed
motor, driven in turn by power from a variable speed AC generator.
The generator is driven from a power take-off from the engine of the
spraying aircraft, a drive assembly includes a device for
controlling the speed of the generator relative to the speed of the
engine. The particularly convenient drive assembly between the
generator and the power take-off is a hydraulic motor, which drives
the generator, driven by a hydraulic pump driven from the power
take-off. The speed of the hydraulic motor can be controllably
varied. Conveniently the AC motor is a synchronous motor.
Laminar
microjet atomizer and method of aerial spraying of liquids
United States Patent / 4,412,654 Yates / November 1, 1983
http://patft.uspto.gov/
A laminar microjet
atomizer and method of aerial spraying involve the use of a
streamlined body having a slot in the trailing edge thereof to
afford a quiescent zone within the wing and into which liquid for
spraying is introduced. The liquid flows from a source through a
small diameter orifice having a discharge end disposed in the quiet
zone well upstream of the trailing edge. The liquid released into
the quiet zone in the slot forms drops characteristic of laminar
flow. Those drops then flow from the slot at the trailing edge of
the streamlined body and discharge into the slipstream for free
distribution.
ROCKET
HAVING BARIUM RELEASE SYSTEM TO CREATE ION CLOUDS IN THE UPPER
ATMOSPHERE
United States Patent: - US3813875 / Issued/Filed Dates: June 4, 1974
/ April 28, 1972
http://pub8.ezboard.com/
A chemical system
for releasing a good yield of free barium (Ba°) atoms and barium
ions (BA+) to create ion clouds in the upper atmosphere and
interplanetary space for the study of the geophysical properties of
the medium. Inventor(s): Paine; Thomas O. Administrator of the
National Aeronautics and Space Administration with respect to an
invention of , Hampton, VA 23364
NASA:
BARIUM - Chemical Formulas/Suppliers
source: gisgaia
This is the "Description of Preferred Embodiments" link in
the NASA Barium Patent listed above. Astounding that this
information was generated in l969 and now,30 years later, there is
evidence of Barium saturation in our atmosphere.
The Barium/Fuel
mixtures are listed below along with the suppliers.
Description
of Preferred Embodiments:
Referring
now to the drawings and more particularly to FIG. 1, there is shown
a segment of a suitable carrier vehicle 10, such for example a
rocket motor. Vehicle 10 is employed to carry fuel tank 11,
insulated oxidizer tank 13 and combustion chamber 15, along with the
necessary instrumentation, from earth into the upper atmosphere or
into interplanetary space. Fuel tank 11 is in fluid connection with
combustion chamber 15 and oxidizer tank 13 is in fluid connection
with combustion chamber 15 by way of respective conduits 17 and 19.
A pair of valves 21 and 23 are disposed within the respective
conduits 17 and 19. Valves 21 and 23 are adapted to be selectively
and simultaneously opened by a suitable battery-powered timing
mechanism, radio signal, or the like, to release the pressurized
fuel and oxidizer from tanks 11 and 13. The fuel and oxidizer then
flow through conduits 17 and 19 and impinge upon each other through
a centrally positioned manifold and suitable jets (not shown) in
combustion chamber 15 where spontaneous ignition occurs. The
reaction products are then expelled through the open ends of
combustion chamber 15 as plasma which includes the desired barium
neutral atoms and barium ions as individual species.
The fuel utilized
in fuel tank 11 is either hydrazine (N2 H4) or liquid ammonia (NH3)
while the oxidizer employed is selected from the group consisting of
liquid fluorine (F2), chlorine trifluoride (ClF3) and oxygen
difluoride (OF2). When using hydrazine as the fuel, barium may be
dissolved therein as barium chloride, BaCl2, or barium nitrate,
Ba(NO3)2, or a combination of the two. When using liquid ammonia as
the fuel, barium metal may be dissolved therein. The combination
found to produce the highest intensity of Ba° and Ba+ resonance
radiation in ground based tests involved a fuel of 16 percent
Ba(NO3)2, 17 percent BaCl2 and 67 percent N2 H4 ; and as the
oxidizer, the cryogenic liquid fluorine F2 and in which an oxidizer
to fuel weight ratio was 1.32.
Other combinations of ingredients tested are set forth in Table I
below:
TABLE I
__________________________
System Optimum O/F Percent
Ionization
Calculated
__________________________
16.7% BaCl2 -
83.3% N2 H4 /ClF3
2.36 68.0
26% BaCl2 -
74% N2 H4 /ClF3
2.08 70.0
50% Ba(NO3)2 -
50% NH3 /ClF3
1.52 -
42.9% Ba(NO3)2 -
57.1% N2 H4 /ClF3
1.19 50.0
16.7% BaCl2 -
83.3% N2 H4 /F2
1.95 68.8
26% BaCl2 -
74% N2 H4 /F2
1.71 70.6
21% BaCl2 -
9% Ba(NO3)2 -
70% N2 H4 /F2
1.57 68.5
17% BaCl2 -
16% Ba(NO3)2 -
67% N2 H4 /F2
1.31 68.1
13% BaCl2 -
21.5% Ba(NO3)2 -
65.5% N2 H4 /F2
1.34 63.7
9% BaCl2 -
30% Ba(NO3)2 -
61% N2 H4 /F2
1.04 63.7
42.9% Ba(NO3)2 -
57.1% N2 H4 /F2
0.976 43.0
42.9% Ba(NO3)2 -
57.1% N2 H4 /OF2
0.694 46.9
26% BaCL2 -
74% N2 H4 /OF2
1.22 52.8
______________________________________
The conditions under which each of the combinations listed in Table
I were tested were ambient and the percentage ionization was
calculated by equations set forth in NASA Contract Report CR-1415
published in August 1969.
The chemical supplier and manufacturers stated purity for the
various chemicals employed are set forth in Table II below:
_______________
Chemical
Supplier Purity
_______________
N2 H4
Olin Mathieson Chemical
Technical Grade
Company, Lake Charles,
97-98% N2 H4
Louisiana (2-3% H2 O)
NH3
Air Products and Chemicals
Technical Grade
Allentown, Pa.
BaCl2
J. T. Baker & Co. Reagent Grade
Phillipsburg, N.J.
Ba(NO3)2
J. T. Baker & Co. Reagent Grade
Phillipsburg, N.J.
F2 Air Products
& Chemicals
98%
Allentown, Pa.
ClF3
Allied Chemical Co.
99.5%
Baton Rouge, La.
OF2
Allied Chemical Co.
98%
Baton Rouge, La.
______________________________________
A solubility study
of various mixtures containing Ba(NO3)2, BaCl2 and N2 H4 was made at
room temperature and is shown in the triangular plot of FIG. 2.
Seven solutions that were used in the tests enumerated in Table I
are indicated by reference letters in FIG. 2 as follows:
a. 16.7% BaCl2 - 83.3% N2 H4
b. 26% BaCl2 - 74% N2 H4
c. 21% BaCl2 - 9% Ba(NO3)2 - 70% N2 H4
d. 17% BaCl2 - 16% Ba(NO3)2 - 67% N2 H4
e. 13% BaCl2 -21.5% Ba(NO3)2 -65.5% N2 H4
f. 9% BaCl2 - 30% Ba(NO3)2 - 61% N2 H4
g. 42.9% Ba(NO3)2 - 57.1% N2 H4
A mixture below the
Saturation Line, that is toward the Ba(NO3)2 or BaCl2 corners
contained a solid and a solution phase whereas the salts were in
complete solution above the saturation line.
All fuel mixtures or systems described were easily handled except
the 50 percent Ba(NO3)2 -50 percent NH3 system. This system caused
clogging of the feed valves due to precipitation of the Ba(NO3)2. In
addition the light values obtained using this system was relatively
low.
In testing of each
of the fuel mixtures set forth in Table I the Ba° light was greater
than the Ba+ light for a given oxidizer/fuel ratio in each of the
mixtures. The maximum light occurred in all systems at a point
located between the stoichiometric O/F and 3 percent less than the
stoichiometric O/F. The stoichiometric O/F is defined as being
equivalent to the oxidizer to fuel weight ratio in a balanced
equation assuming the salt is converted to free Ba, F to HF, Cl to
HCl and O to H2 O. For example, one system tested had an O/F ratio
of 142 grams oxidizer per 100 grams fuel or 1.42/1.00. If the barium
is assumed to be converted to BaF2 then the stoichiometric O/F is
1.47. Since the greatest light output in all cases occurred with O/F
less than stoichiometric it is apparent that little of the Ba was
combined as BaF2 or BaCl2. This was confirmed by spectrographic
analysis.
In Table II the various systems are listed in decreasing light
output or relative light intensity as measured by phototubes in
millivolts, thereby indicating the relative barium yield.
TABLE III
__________________________________________________________
SYSTEM MAXIMUM RELATIVE
(percent weight for fuel)
INTENSITY, millivolts
Ba° 5535 A
Ba+ 4554 A
_____________________________________________
17% BaCl2 -16% Ba(NO3)2 -67% N2 H4 /F2
27600
11800
13% BaCl2 -21.5% Ba(NO3)2 -65.5% N2 H4 /F2
23600
8340
21% BaCl2 -9% Ba(NO3)2 -70% N2 H4 /F2
20600
9100
9% BaCl2 -30% Ba(NO3)2 -61% N2 H4 /F2
16600
5970
26% BaCl2 -74% N2 H4 /F2
16600
6520
26% BaCl2 -74% N2 H4 /OF2
11800
2100
16.7% BaCl2 -83.3% N2 H4 /F2
9100 3350
42.9% Ba(NO3)2 -57.1% N2 H4 /F2
9000 1800
42.9% Ba(NO3)2 -57.1% N2 H4 /OF2
7300 1330
42.9% Ba(NO3)2 -57.1% N2 H4 /ClF3
663 94
50% Ba(NO3)2 -50% NH3 /ClF3
221 44
______________________________________________
From the above
information, it is readily seen that the 17 percent BaCl2 -16
percent Ba(NO3)2 -67 percent N2 H4 /F2 system gave the greatest
amount of light intensity of the 4554 A Ba+ and 5535 A Ba° spectral
lines. Ambient tests showed that the optimum oxidizer to fuel ratio
of this system was 1.32 to 1.00. This system containing 8.52 weight
percent barium was estimated to be 68.1 percent ionized. Also since
this system had the largest relative light intensity it would be
expected to give the greatest amount of Ba° and Ba+ and would
appear to be the optimum system for a barium payload. In all systems
tested it was found that the relative light reached a maximum at the
O/F corresponding to the stoichiometric equation yielding barium as
one of the reaction products and that the relative light output was
sensitive to the O/F. Moving to either side of the optimum O/F
caused a sharp decrease in relative light.
In vacuum tests the
ignition of each system tested was smooth and like the ambient tests,
took place in the combustion chamber. The rapid expansion in vacuum
caused a decreased atom and ion density in the luminous flame which
caused the light intensity to be about 1/37 to 1/50 the intensity
measured in ambient tests. The percentage ionization was
approximately the same for vacuum and ambient tests.
The operation of
the invention is now believed apparent. Initially, fuel tank 11 is
charged with the fuel containing the desired quantity of dissolved
barium salt and pressurized with helium. The fuel tank pressure may
be in the range of 6.89 to 20.06 ¥ 105 Newton/meter2. Oxidizer tank
13 is also charged with the appropriate oxidizer and pressurized.
Cryogenic oxidizers such as OF2 and F2 are condensed from gases in
the closed oxidizer tank which must be maintained enclosed in a
liquid nitrogen bath. The oxidizer feed valve 23 and conduit 19 must
also be maintained at liquid nitrogen temperature with a liquid
nitrogen jacket when employing a cryogenic oxidizer.
The noncryogenic oxidizer, ClF3, may be pressurized into the closed
oxidizer tank 13 from a supply bottle with super dry nitrogen.
Combustion chamber 15 is formed of stainless steel, aluminum, or the
like F2 compatible metals and is internally partitioned by the
manifold, not shown. The conduits 17 and 19 terminate in a manifold
having injector orifices (not shown) mounted 90° to each other
within each end of chamber 15 and sized for pressure drops of 5.24
to 10.2 ¥ 105 Newton/meter2 across the orifice. Fuel and oxidizer
flows are in the range of 2.05 to 6.82 Kg/sec each. The entire
system is carried into the upper atmosphere or interplanetary space
by rocket vehicle 10 where, in response to a suitable signal, timing
mechanism or the like, valves 21 and 23 may be selectively opened
and closed and the pressurized liquid fuel and oxidizer will flow
through conduits 17 and 19 into combination unit 15. When the
hypergolic liquids impinge upon each other, they spontaneously
ignite to expel reaction product gases or plasma including the
highly luminous barium neutral atoms and barium ions as individual
species. All of the barium reaching the combustion chamber is
vaporized and released through the opposite ends thereof so that a
high yield efficiency is obtained. The resulting high flame
temperature, approximately 4,000°K., and some as yet not determined
chemical activation, produces a relatively large amount of barium
ions in the flame which is a highly desirable condition. It has been
estimated from spectroscopic measurements that the degree of
ionization may be as high as 75 percent in the released plasma in
comparison to being on the order of 1 percent for the previously
used Ba-CuO solid system which depends almost entirely on solar
photoionization, a time-dependent phenomena which further reduces
the usable barium yield of this known system.
Thus, it is readily
apparent that the present invention provides an inherently more
efficient process of producing barium clouds wherein the degree of
ionization in the released plasma is much greater. The selectively
opening and closing of valves 21 and 23 gives the possibility of a
payload with multiple releases permitted due to the start and stop
capabilities of the liquid system. Also, the liquid system of the
present invention gives the possibility of controlling rates so that
a trailtype release can be obtained as well as a point-source type.
In addition, the liquid system of the present invention effects the
formation of barium atoms and ions at the time of combustion and
expansion at high temperatures and results in little opportunity for
the barium to condense during release.
There are obviously
many variations and modifications to the present invention that will
be readily apparent to those skilled in the art without departing
from the spirit or scope of the disclosure or from the scope of the
claims.
Quelle (source): http://www.lightwatcher.com/
Informant: George
Paxinos
Link: http://www.chemtrailcentral.com
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