WFC 417 — WFC 417

Page 0

memo WFC417

Water Fuel Cell

Hydrogen Fracturing Process

How To Use Voltage To Stimulate The Water Molecule To Produce Atomic Rocket-Fuel On Demand

Inventor:

WATER FUEL CELL Stanley A. Meyer »,2a 3792 Broadway

Grove City, Ohio 43123

JESUS CHRIST 18 LORD

Copyright © 1983 in U.S.A. By Stanley A. Meyer © under UCC 1987 By Stanley A. Meyer U.S. and Foreign Patents Pending

Page 1

RE: Water Powered Rocket Engine memo WFC417 Data Reference: WFC Tech-Brief

Method: Using Voltage to stimulate the water molecule to produce Atomic Rocket-Fuel on Demand.

Operational Parameters

RESONANT CHARGING CHOKE (c) (b) (RESISTIVE COIL-WIRE R2)

VARIABLE

rOTiOV be EXCITOR-ARRAY (ER)

SECONDARY

PICKUP COIL (A) (GAPAGITOR)

(RESISTIVE WIRE-COIL R1)

NATURAL WATER

(DIELECTRIC LIQUID)

IMUM:

PRIMARY

COIL (g)

Me souarepsiecraca, tf) S -Tunepe

ISOLATED N

PULSING-TRANSFORMER CHOKE (d)

(RESISTIVE COIL-WIRE R3)

Coprright © 1981 By Stanley A. Meyer

Figure 1 - 1. Voltage Intensifier Circuit (AA)

Stanley A. Meyer Page_1 of 28

Page 2

RE: Water Powered Rocket Engine memo WFC417

CIRCUIT COMPONENT INTERACTION

PULSING TRANSFORMER (G)

The pulsing transformer (G) steps up voltage amplitude or voltage potential during pulsing operations. The primary coil is electrically isolated (no electrical connection between primary and secondary coil) to form Voltage Intensifier Circuit (AA). Voltage amplitude or voltage potential is increase when secondary coil is wrapped with more turns of wire. Isolated electrical ground (J) prevents electron flow from input circuit ground.

BLOCKING DIODE (B)

Blocking Diode (B) prevents electrical " shorting " to secondary coil (A) during pulse-off time since the diode "only" conducts electrical energy in the direction of the schematic arrow.

LC CIRCUIT

FIGURE 1 - 2. LC CIRCUIT SCHEMATIC

Resonant Charging Choke (c) in series with Excitor-array (E1/E2) forms an inductor-capacitor circuit (LC) since the Excitor-Array (ER) acts or performs as an capacitor during pulsing operations.

The high Dielectric Properties (insulator to the flow of amps) of natural water (dielectric constant being 78.54 @ 25C) between the electrical plates (E1/E2) forms the capacitor (ER). Water now becomes part of the Voltage Intensifier Circuit in the form of "resistance" between electrical ground and pulse-frequency positive-potential...helping to prevent electron flow within the pulsing circuit (AA) of Figure 1-1).

‘The Inductor (C) takes-on or becomes an Modulator Inductor which steps up an oscillation of an given charging frequency with the effective capacitance of an pulse-forming network in order to charge the voltage zones (E1/E2) to an higher potential beyond applied voltage input.

The Inductance (C) and Capacitance (ER) properties of the LC circuit is therefore "tuned" to resonance at a certain frequency. The Resonant Frequency can be raised or lowered by changing the inductance and/or the capacitance values. The established resonant frequency is, of course, independent of voltage amplitude, as illustrated in Figure 9BB as to Figure 16A.

The value of the Inductor (C), the value of the capacitor (ER), and the pulse-frequency of the | voltage being applied across the LC circuit determines the impedance of the LC circuit.

Stanley A. Meyer Page_2 of 28

Page 3

RE: Water Powered Rocket Engine memo WFC417

VARIABLE ANALOG VOLTAGE AMPLITUDE

PULSE TRAIN

fm ae; | apaae

ANALOG

VOLTAGE

ACROSS PLATES

STEP CHARGING

EFFECT

PULSE TIME ——

FIG. 9BB: APPLIED VOLTAGE TO PLATES

COPYRIGHT © 1981 BY STANLEY A. MEYER

Stanley A. Meyer Page_3 of 28

Page 4

VARIABLE ANALOG VOLTAGE AMPLITUDE

RE: Water Powered Rocket Engine memo WFC417 | Vn 53 53a PULSE TRAIN

PULSE TIME

FIG. 16A: APPLIED VOLTAGE TO RESONANT CAVITY

COPYRIGHT © 1982 BY STANLEY A. MEYER

Stanley A. Meyer Page_4 of 28 |

Page 5

RE: Water Powered Rocket Engine memo WFC417

The impedance of an inductor and a capacitor in series, Z cerieg is given by Z series = (Xo - XL)

Where

The Resonant Frequency (F) of an LC circuit in series is given by

Ohm's Law for LC circuit in series is given by

LC VOLTAGE

The voltage across the inductor (C) or capacitor (ER) is greater than the applied voltage (H). At frequency close to resonance, the voltage across the individual components is higher than the applied volatge (H), and, at resonant frequency, the voltage Vt across both the inductor and the capacitor are theoretically infinite, However, physical constraints of components and circuit interaction prevents the voltage from reaching infinity.

The voltage (Vj) across the inductor (C) is given by the equation

Stanley A. Meyer Page_5 of 28.

Page 6

RE: Water Powered Rocket Engine memo WFC417

The voltage (Vc) across the capacitor is given by

During resonant interaction, the incoming unipolar pulse-train (H) of Figure (1-1) as to Figure

(9B) produces an step-charging voltage-effect across Excitor-Array (ER), as illustrated in Figure (9BB) and Figure (16A). Voltage intensity increases from zero "ground-state" to an high positive voltage potential in an progressive function. Once the voltage-pulse is terminated or switch-off, voltage potential returns to "ground-state" or near ground-state to start the voltage deflection process

over again.

Voltage intensity or level across Excitor-Array (ER) can exceed 20,000 volts due to circuit (AA) interaction and is directly related to pulse-train (H) variable amplitude input.

RLC CIRCUIT

Inductor (C) is made of or composed of resistive wire (R2) to further restrict D.C. current flow beyond inductance reaction (XL), and, is given by

Dual-inline RLC NETWORK

Variable inductor-coil (D), similar to inductor (C) connected to opposite polarity voltage zone (E2) further inhibits electron movement or deflection within the Voltage Intensifier Circuit. Moveable wiper arm fine "tunes" "Resonant Action" during pulsing operations. Inductor (D) in relationship to inductor (C) electrically balances the opposite voltage electrical potential across voltage zones (E1/E2).

VIC RESISTANCE

Since pickup coil (A) is also composed of or made of resistive wire-coil (R1) , then, total circuit resistance is given by

Where, Rp is the dielectric constant of natural water

Stanley A. Meyer Page_6 of 28

Page 7

RE: Water Powered Rocket Engine memo WFC417

FIG. 9B: VARIABLE AMPLITUDE UNIPOLAR

PULSE VOLTAGE FREQUENCY SUPER IM-

POSED ONTO AN 50% DUTY-CYCLE PULSE-

TRAIN DYNAMICALLY CONTROLS THE

HYDROGEN GAS-RATE WHILE RESTRIC-

TING AMP FLOW.

Copyright © 1981 by Stanley A Meyer

Stanley A. Meyer Page_7 of 28

Page 8

RE: Water Powered Rocket Engine

Ohm's Law as to applied electrical power, which is

memo WFC417

NEGATIVE

ELECTRICAL

POTENTIAL

Where

Whereby

Electrical power (P) is an linear relationship between two variables, voltage (E) and AMPS

VOLTAGE DYNAMIC

ELECTRICAL

ATTRACTION REPELLING

FORCE ELECTRICAL

POSITIVE Bence

ELECTRICAL

FIELD

ELECTRON

POSITIVE PULSING DEFLECTION

CIRCUIT

Figure 1-3. Voltage Potential Difference

POTENTIAL ENERGY

Voltage is "electrical pressure" or "electrical force" within an electrical circuit and is known as "voltage potential". The higher the voltage potential, the greater "electrical attraction force" or "electrical repelling force" is applied to the electrical circuit. Voltage potential is an "unaltered" or "unchanged" energy-state when "electron movement" or

"electron deflection" is prevented or restricted within the electrical circuit.

VOLTAGE PERFORMS WORK

Unlike voltage charges within an electrical circuit set ups an "electrical attraction force"; whereas, like electrical charges within the same electrical circuit encourages an "repelling action". In both cases, electrical charge deflection or movement is directly related to applied voltage. These electrical "forces" are known as "voltage fields" and can exhibit either a positive or negative

electrical charge.

Stanley A. Meyer Page_8 of 28

Page 9

RE: Water Powered Rocket Engine memo WFC417

Likewise, Ions or Particles within the electrical circuit having unlike electrical charges are attracted to each other. Ions or particles mass having the same or like electrical charges will move away from one another, as illustrated in Figure 1-3.

Furthermore, electrical charged ions or particles can move toward stationary voltage fields of opposite polarity, and, is given by Newton's second Law

ioe a

Where

The acceleration (A) of an particle mass (M) acted on by a Net Force ®.

Whereby

Net Force €) is the "electrical attraction force" between opposite electrically charged entities, and, is given by Coulomb's Law

Whereas

Difference of potential between two charges is measureed by the work necessary to bring the charges together, and, is given by

The potential at a point due to a charge (q) at a distance (R) in a medium whose dielectric constant is (e).

Stanley A. Meyer Page_9 of 28

Page 10

RE: Water Powered Rocket Engine memo WFC417

ATOMIC INTERACTION TO VOLTAGE STIMULATION

ORBITAL NUCLEUS

ELECTRONS ~~ (PROTONS / NEUTRONS)

NEGATIVE

ELECTRICAL

CHARGE

POSITIVE ELECTRICAL

CHARGE

STABLE - STATE

Figure 1-4. Electrical Charges of an Atom

Atomic structure of an atom exhibits two types of electrical charged mass-entities, orbital electrons having negative electrical charges (- ) and an Nucleus (at least one proton) having an positive electrical charged ( + ) . The positive electrical charge of the Nucleus equals the sum total of all negative electrical charged electrons when the Atom is in "stable-state".

In stable-state or normal-state, the number of electrons equals the number of protons to give the atom "NO" net electrical charge.

Whenever one or more electrons are "dislodged" from the atom, the atom takes-on a net positive electrical charge and is called an positive ion. If an electron combines with an stable or normal atom, the atom has a net negative charge and is called a negative ion.

Voltage potential within an electrical circuit can cause one or more electrons to be dislodged from the atom due to opposite electrical polarity attraction between unlike charged entities, as shown in Figure 20F (see Figure 1-3 again) as to Newton's and Coulomb's Laws of

Newton's and Coulomb's Laws of electrical-force is used to combine or join atoms together by way of Covalent Bonding (sharing electrons between atoms) to form a molecule of gas, liquid, or solid.

The liquid molecule of water is formed when the two Hydrogen atoms takes-on a net "positive electrical charge" , which is, equal to the net "negative electrical charge" of the Oxygen atom. The opposite electrical force (qq') between the Hydrogen and Oxygen atoms keeps the water molecule intact when the sharing of electrons move from one atom structure to another. The strength of the electrical attraction force (qq' ) between the water molecule atoms is determined by the electrical-size of the hydrogen atoms and the displacement of the negative charged electrons during covalent sharing.

Stanley A. Meyer Page 10 of 28

Page 11

Johey ‘y Agjueyg

THERMAL EXPLOSIVE a AS

ENERGY NEGATIVE CHARGED!

LIBERATED ‘@)

ELECTRON ELECTRONS Sy, mehr tag: 5 DEFLECTION ~ 1 Byeerion (POSITIVE CHARGED) _ — -“\_ cere ae S a \ oo LIGHT ' ul ABSORPTION

NUCLEI” ~ ~ es e 5 —_ ENERGY - ELECTRON

DECAY i. ect Be B Z SUB-LEVELS ENT

| ims

PHOTON ENERGY erecrioes

INJECTION PULSE VOLTAGE

FREQUENCE INJECTION

7. T = GAS THERMAL IGNITION =a lai

FIG. 20F: HYDROGEN FRACTURING PROCESS

COPYRIGHT © 1983 BY STANLEY A. MEYER

ouidugq 1oFI0y poromog J31e@ AA “TY

LIvOAM OulouT

Page 12

RE: Water Powered Rocket Engine memo WFC417

VOLTAGE DISSOCIATION OF THE WATER MOLECULE

POSITIVE NEGATIVE

ELECTRICAL VOLTAGE

POTENTIAL POTENTIAL

LIBERATED (-)

\ (+) ELECTRONS

H20 MOLECULE /

ELECTRICAL

COPYRIGHT © 1981 BY STANLEY A. MEYER

Figure 1-5. Electrical Polarization Process

Placement of an pulse-voltage potential across the Excitor-Array (ER) while inhibiting or preventing electron flow within the Voltage Intensifier Circuit (AA) causes the water molecule to separate into its component parts by, momentarily, pulling away orbital electrons from the water molecule, as illustrated in Figure 1-5.

The stationary " positive" electrical voltage-field (E1) not only attracts the negative charged oxygen atom but also pulls away negative charged electrons from the water molecule. At the same time, the stationary "negative" electrical voltage field (E2) attracts the positive charged hydrogen atoms. Once the negative electrically charged electrons are dislodged from the water molecule, covalent bonding (sharing of electrons) ceases to exsist, switching-off or disrupting the electrical attraction force (qq*) between the water molecule atoms.

The liberated and moving atoms (having missing electrons) regain or captures the free floating electrons once applied voltage is switch-off during pulsing operations. The liberated and electrically stabilized atom having a net electrical charge of "zero" exit the water bath for hydrogen gas utilization.

Dissociation of the water molecule by way of voltage stimulation is hereinafter called "The Electrical Polarization Process".

Subjecting or exposing the water molecule to even higher voltage levels causes the liberated atoms to go into an "state" of gas ionization. Each liberated atom taking-on its own "net" electrical charge. The ionized atoms along with free floating negative charge electrons are, now, deflected (pulsing electrical voltage fields of opposite polarity) through the Electrical Polarization Process...imparting or superimposing a second physical-force (partiicle impact) unto the electrically charged water bath. Oscillation (back and forth movement) of an electrically charged particles by way of Voltage deflection is hereinafter called "Resonant Action", as illustrated in Figure 12.

Attenuating and adjusting the " pulse-voltage-amplitude" with. respect to the " pulse volyage frequency", now, produces hydrogen gas on demand while restricting amp flow from the power supply input.

Stanley A. Meyer Page 12 of 28

Page 13

RE: Water Powered Rocket Engine

HIGH TEMPERATURE

FLAME

FLAME IGNITOR

n-B-— ELECTRICAL

VOLTAGE ZONE.

GEOMETRICAL (AMP RESTRICTED)

PROGRESSION

OF GASES

NE RESONANT CAVITY

AMP INHIBITOR CRK'T SS

B+ ELECTRICAL VOLTAGE ZONE

(AMP RESTRICTED)

FIG. 12: ELECTRICAL VOLTAGE ZONES

(B-/B+) FORMING A RESONANT-CAVITY

Copyright * 1982 by Stanley A Meyer memo WFC417

Stanley A. Meyer Page.13 of 28°

Page 14

RE: Water Powered Rocket Engine memo WFC417

LASER INTERACTION

Nec

Laser eo L3yW27%_—_ Energy

FIGURE 1-6. Led Cluster-Array

Light -emitting diodes arranged in an Cluster-Array provides and emits an narrow band of visible light energy into the voltage stimulated water bath, as illustrated in Figure 19 as to Figure 18. The absorbed Laser Energy (ELECTROMAGNETIC ENERGY) causes many atoms to lose electrons while highly energizing the liberated combustible gas ions prior to-and during thermal gas-ignition. Laser or light intensity is linear with respect to the forward current through the LEDS, and, is determined by

Vin — Vled

Ted

Where

I jeq is the specified forward current (typically 20ma. per diode); V jeg is the LED voltage drop (typically 1.7 volts for red emitters).

Ohm's Law for LED circuit in parrallel array, and, is given by

Pwatts = Veco It

Where

I, is the forward current through LED cluster-Array; Vo¢ is volts applied (typically 5 volts). Stanley A. Meyer Page 14 of 28

Page 15

RE: Water Powered Rocket Engine memo WFC417 ene os execTacAL

LTAGE ZONE

(AMP RESTRICTED) (AMP RESTRICTED)

ELECTRICALLY

PPOSITE POLARITY

ATTRACTION CHARGED ATOMS AMP INHIBITOR

CIRCUIT

FIG. 18: PHOTON ENERGY AIDS RESONANT-ACTION

Copyright © 1983 by Stanley A. Meyer Stanley A. Meyer Page15 of 28_

Page 16

RE: Water Powered Rocket Engine memo WFC417

TIMER SWEET! WATER INLET

CONTROL

PULSE jy ~

CONTROL

= = RESONATE

CAVITY

4% AMP INHIBITOR

VOLTAGE AMPLITUDE—

CIRCUIT

FREQUENCY CONTROL

FIG. 19: LASER INJECTED RESONANT-CAVITY

Copyright © 1983 by Stanley A Meyer Stanley A. Meyer Page16 of 28

Page 17

RE: Water Powered Rocket Engine memo WFC417

Whereby

Laser or light intensity is varaiable as to duty cycle on/off pulse-frequency from lh, to 65 h,

and above, and, is given by

Le is light intensity in watts; Tj is current on-time; T3 is current off-time; and (ION) = RMS value of load current during on-period.

Injecting Laser Energy into the Electrical Polarization Process and controlling the intensity of that light-energy causes the Combustible gases to reach an higher energy-state (electromagnetically priming the combustible gas ions) which, in turns, accelerates gas production while raising gas-flame temperature beyond "normal" gas-burning levels.

Injecting "Electromagnetically Primed" and "Electrically Charged" combustible gas ions (from water) into other light-activated Resonant Cavities further promotes gas-yield beyond voltage/laser stimulation, as illustrated in Figure 20D as to Figure 20.

ELECTRON EXTRACTION PROCESS

RESONANT CHARGING CHOKE (c)

ALTERNATE R BLOCKING (RESISTIVE COIL-WIRE R7)

SWITCH (Q)

VARIABLE PULSE é )

VOLTAGE FREQUENCY (K) b f ise

LASER ENERGY

Bee conciantic INJECTION (V)

DEVICE (S)

may (FILAMENT-WIRE R5)

COIL (L)

COMBUSTIBLE

GAS INPUT (2)

PICKUP COIL (N)

(RESISTIVE WIRE-COIL R4)

ISOLATED PULSING :

TRANSFORM AMP INHIBITOR (Y)

sah (RESISTIVE WIRE-COIL R6)

Copyright © 1982 By Stanley A. Meyer

FIG. 1-7. ELECTRON EXTRACTION CIRCUIT (BB)

Stanley A. Meyer Page17 of 28

Page 18

RE: Water Powered Rocket Engine memo WFC417

VARIABLE

POWER

SUPPLY GAS EXIT

Bil

(SERIES AND/OR

PARALLEL ARRAY) ~ Ny

PULSE

FREQUENCY

CONTROL

SEQUENTIAL

GATE

CONTROL

VOLTAGE INTENSIFIER

SYNC PULSE

PULSING

LASER

(LIGHT ENERGY)

FIBEROPTIC

BUNDLE

(LIGHT PATHWAY)

FIG. 20D: POWER LOAD DISTRIBUTION

COPYRIGHT © 1982 BY STANLEY A. MEYER

Stanley A. Meyer Page18 of 28.

Page 19

RE: Water Powered Rocket Engine

memo WFC417

. SUPER

ROCKET FLAME

ATOMIC

GAS GUN

RESONANT ATOM

er QUENCHING AVI

CIRCUIT NOZZLE

MODULAR

ASSEMBLY

FIG.20: ATOM INJECTED RESONANT-CAVITY

(INTERLOCKING MODULES)

COPYRIGHT © 1986 BY STANLEY A. MEYER

Stanley A. Meyer

Page 20

RE: Water Powered Rocket Engine memo WFC417

Exposing the displaced and moving combustible gas atoms (exiting water bath and passing through Gas Resonant Cavity (T), Figure 20JX as to Figure 20H) to another or separate pulsating laser energy-source (V) at higher voltage levels (E3/E4) causes more electrons to be “pulled away" or "dislodged" from the gas atoms, as illustrated in Figure 1-8 as to Figure

20F. The absorbed Laser Energy "forces" or "deflects" the electrons away from the gas atom nucleus during voltage-pulse Off-Time. The reoccurring positive voltage-pulse (K) attracts (qq') the liberated negative electrically charged electrons to positive voltage zone (E3). While, at the same time, the pulsating negative electrical voltage potential (E4) attracts (qq') the positive electrical charged nucleus. The Positive Electrical Voltage Field (E3) and Negative Electrical Voltage Fields (E4) are triggered SIMULTANEOUSLY during the same duty-pulse.

NEGATIVE

ELECTRICAL ELECTRICAL

POTENTIAL POTENTIAL

GAS RESONANT LIBERATED

CAVITY ELECTRONS (-),4

= = ORBITAL 4,

os ae a Ng ECTRONS 4,

ABSORBED \\ E4

LASER

ENERGY M

me yal \\

ELECTRICAL COMBUSTIBLE

ATTRACTION-FORCE GAS IONS

Copright © 1982 By Stanley A. Meyer

Fig. 1-8. DESTABILIZING COMBUSTIBLE GAS IONS

Stanley A. Meyer Page 20 of 28

Page 21

RE: Water Powered Rocket Engine memo WFC417

EXPELLED

ELECTRICALLY CHARGED

AND PRIMED COMBUSTIBLE

GAS IONS

VOLTAGE

INTENSIFIER

HOUSING

LASER

PULSING

POSITIVE a) —

VOLTAGE

ZONE

LIGHT

CHAMBER

OPTICAL

LIGHT TRANSFER

LENS

UUW

sae

= SEMICONDUCTOR

NEGATIVE yr |) LASER WITH — nar He LENS CAP

ELECTRICAL

POWER INPUT TO

LASER ASS'Y

VARIABLE

PULSE VOLTAGE

FREQUENCY

INPUT *, COMBUSTIBLE

GAS INPUT

FIG. 20JX: GAS RESONANT CAVITY

COPYRIGHT © 1983 BY STANLEY A. MEYER

Stanley A. Meyer Page 21 of 28

Page 22

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Page 23

RE: Water Powered Rocket Engine memo WFC417

Electron Extraction Circuit (BB) of Figure 1-7 removes, captures, and consumes the " dislodged" electrons (from the gas atoms) to cause the gas atoms to go into and reach "Critical-State", forming highly energized combustible gas atoms having missing electrons. Resistive values (R4,R6, R7, and dielectric constant of gas Rg) and isolated electrical ground (W) prevents "electron-flow" or "electron deflection" from occurring within circuit (BB) during pulsing operations (at resonant frequency) and, therefore, keeps the gas atoms in Critical-State by "NOT" allowing electron replacement to occur or take place between the moving gas atoms. The "dislodged" negative charged electrons are "destroyed" or "consumed" in the form of "heat" when Amp Consuming Device (S) (such as an light bulb) is positive electrically energizied during alternate pulsing operations. Laser activated or laser primed gas ions repels the "dislodge" electrons being consumed, as illustrated in Figure 20F as to Figure 20G. The Electron Extraction Process (BB) is, hereinafter, called "The Hydrogen Gas Gun" and is placed on top of an Resonant Cavity Assembly, as illustrated in Figure 20JX as to Figure 20H.

THERMAL EXPLOSIVE ENERGY

OXYGEN ATOM i aes

ELECTRONS

ELECTRON

ee MISSING

ELECTRONS

ELECTRICAL

ABSORBED ATTRACTION-FORCE

COVALENT

THERMAL az

HYDROGEN ATOM

HYDROGEN ATOM

Copyright © 1982 By Stanley A. Meyer

Fig.1-9. HYDROGEN FRACTURING PROCESS

Stanley A. Meyer Page. 23 of 28

Page 24

memo WFC417

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Page 24 of 2

Stanley A. Meyer

Page 25

RE: Water Powered Rocket Engine memo WFC417

Exposing the expelling " Laser-Primed" and "Electrically Charged" combustible gas ions (exiting from Gas Resonant Cavity) to an thermal-spark or heat-zone causes thermal gas-igition, releasing thermal explosive energy (gtnt) beyond the Gas-Flame Stage, as illustrated in Figure 20E as to 20H.

Thermal Atomic interaction (gtnt) is caused when the combustible gas ions (from water) fail to unite or form an Covalent Link-up or Covalent Bond between the water molecule atoms, as illustrated in Figure 1-9. The oxygen atom having less than four covalent electrons (Electron Extraction Process) is unable to "Reach" "Stable-State" (six to eight covalent electrons required) when the two hydrogen atoms seek to form the water molecule during thermal gas-ignition. The absorbed Laser-energy (Va, Vb, and Vc) weakens the "Electrical Bond" between the orbital electrons and the Nucleus of the atoms. And, electrical attraction-force (qq'), being stronger than "Normal" due to the lack of covalent electrons, "Locks Onto" and "Keeps" the hydrogen electrons. These "abnormal" or "unstable" conditions causes the combustible gas ions to over compensate and breakdown into thermal explosive energy (gtnt). This Atomic Thermal-Interaction between combustible gas ions is now, called "THE HYDROGEN

FRACTURING PROCESS'.

By simply attenuating or varying voltage amplitude in direct relationship to voltage ! pulse-rate determines Atomic Power- Yield under control-state. : |

ROCKET PROPULSION

LIQUID OXYGEN FUEL-TANK |

(LASER PRIMED ATOMS HAVING MISSING ELECTRONS) |

ROCKET FLAME

(EXPLOSIVE THERMAL ENERGY [gtnt] ON DEMAND)

LIQUID TO GAS PASSAGE WAY

(VARIABLE CONTROLLED FLOW-RATE)

ROCKET ENGINE

(GAS MIXING AND COMBUSTION

CHAMBER)

LIQUID HYDROGEN FUEL-TANK

(LASER PRIMED ATOMS)

Copyright © 1982 By Stanley A. Meyer

Fig. 1-10. Atomic Powered Rocket Engine

Stanley A. Meyer Page 25 of 28

Page 26

THERMAL

EXPLOSIVE

ENERGY

(gtn t)

WATER

ATOMS

Stanley A. Meyer

COMBUSTIBLE IONIC

GASES

(PRIMED AND CHARGED)

RE: Water Powered Rocket Engine

VARIABLE

CONTROL

RATE

PHOTON ENERGY

INJECTION

VOLTAGE

VARIABLE INJECTION

CONTROL

RATE

VARIABLE

CONTROL

RATE

a THERMAL GAS

IGNITION

NATURAL WATER =

FIG. 20E: CONTROLLED ENERGY-YIELD

FROM WATER ATOMS

COPYRIGHT © 1983 BY STANLEY A. MEYER

memo WFC417

Page 27

RE: Water Powered Rocket Engine memo WFC417

SUPER

\_ ROCKET FLAME

ENERGY ACCUMULATOR

AND NOZZLE

ATOMIC

GAS GUN

RESONANT

CAVITY

FIG.17: RESONANT-CAVITIES FORMING

THE WATER VESSEL

Copyright © 1982 by Stanley A. Meyer

Stanley A. Meyer Page27 of 28

Page 28

RE: Water Powered Rocket Engine memo WFC417

Add-on Resonant Cavities (placed beneath the Hydrogen Gas Gun Assembly) arranged in parallel to verticle Cluster-Array increases the Atomic Energy-yield of The Hydrogen Fracturing Process undergoing thermal gas-ignition, as illustrated in Figure 17 as to Figure 20. This Cluster-Assembly or Cluster-form is, hereinafter, called "The Water Powered Rocket

Prolong Rocket-Flight carrying heavier pay-loads is achieved by Liquifing the "specially treated" Combustible Gas Ions (laser-primed oxygen gas-atoms having missing electrons and laser-primed hydrogen gas-atoms) under pressure in separate Fuel-Tanks affixed to an "Rocket Engine", as illustrated in Figure 1-10. Rocket-Thrust is, now, controlled by the flow-rate of the Combustible ion gases entering the Combustion Chamber of the Rocket Engine.

The Hydrogen Fracturing Process is an Retrofit Technology and is applicable to all Energy-systems including Aircraft.

Stanley A. Meyer Page 28 of 28°