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Explanation of dynamical Biefeld-Brown Effect
from the standpoint of ZPF field
Takaaki Musha
INTERNATIONAL ACADEMY OF
ASTRONAUTICS
Missions to the outer solar system and
beyond
FIFTH IAA SYMPOSIUM ON REALISTIC
NEAR-TERM
ADVANCED SCIENTIFIC SPACE MISSIONS
Aosta, Italy, July 2-4, 2007
Contents
(1) Purpose
(2) Outline of the dynamical B-B effect
(3) Possibility of artificial gravity induced by
dynamical electromagnetic field
(4) Electrogravitic propulsion systems
(5) Conclusion
Purpose
• To explain the weigh reduction at the
experiment by applying alternate electric field
to the capacitor conducted by the research
group of the HONDA R&D Institute group
from the standpoint of ZPF field in a space
• To investigate the applicability of the
dynamical Biefeld-Brown effect for the
propulsion system
Outline of the dynamical B-B effect
• From the 1st of Feb. till the 1st of March in 1996,
the research group of the HONDA R&D Institute
conducted experiments to verify the B-B effect with
an improved experimental device in 1996 to reject
the influence of corona discharges and electric
wind around the capacitor by setting the capacitor
in the insulator oil contained within a metallic
vessel. They found that the weight loss by the
alternate electric field was greater than the static
case .
Experimental set-up
t=1mm,d=170mm,W=62g
Electrical circuit for generating HV electric field
Schematic diagram of the electric circuit
8kV AC pulse, f=50Hz,
Histogram of weight losses observed at the experiment
gM 63.09.0 ±=∆
Forces generated by the ionic transfer of
the momentum
)/(/2 000 giqVmM ⋅=∆
By introducing experimental values, 1682pF, 8kV, and
50Hz, into the equation, the weight reduction due to ionic
winds becomes 1.3×10-3g , which is negligible small
compared with the experimental result.
T.B.Bahder & C.Fazi
EZEGZE rrg ⋅×−=⋅−≈ −
εεπε 11
0 1062.84
)(002.0/1062.8 0
11
ggEWZM r =×=∆ −
ε
22 ψµεψε SG
d
M
GFg ==
(Musha: weak field approximation of general relativity theory)
(Ivanov: Weyl-Majumdar-Papapetrou solutions of the general
Relativity theory)
Gravitational field generated by the B-B effect
gM 63.09.0 ±=∆(Experiment)
Possibility of artificial gravity
induced by
dynamical electromagnetic field
2
2
2 c
m c
π
ωhΓ
=
ZPF field in a space
ω
π
ω
ωωρ d
c
d 32
3
2
)(
h
=
Inertial mass is originated to the
interaction of sub-elementary
particles with the vacuum ZPF
field
Inertial mass generated by the ZPF field
(M.B.King : Tapping the zero-point energy)
A slight coherence of vacuum fluctuations due
to the high potential electric field caused an
alternation of inertial properties of the body
with the ionic lattice of a rapidly spinning
atom .
(B.Haish, A.Rueda and H.E.Puthoff )
If one could somehow modify the vacuum
medium then the mass of a particle or object in
it would change according to the zero-point
field theory.
><= 2
2
0
2
2
A
cm
e
HA
2
3
0
2
2
cA
cm
e
H ω
π
h
=′
(A) Electrodynamic Hamiltonian by P.Milonni
(B) Electromagnetic Hamiltonian corresponding Zero-point
fields (B.Haisch, A.Rueda, H.E.Puthoff)
Process to derive the anti-gravity equation
A=0
No Electric field
Electric field Impressed
AA HH ′∆=
Initial State
0=AH
)( 0AAA HHH ′−′=′∆
Assumption to derive equation
0)( =′−∆ AA HH
><−=∆ 2
02
A
c
ω
π
ω
h
><
ω
π
=ωω∆−=∆ 2
2
0
0/2/ A
c
mm
h
Electrodynamic Hamiltonian
AA HH ′∆=
Equation of Mass Shift
2
2
2 c
m c
π
ωhΓ
=
r
tNed
cr
crtp
c
A
)(
4
1)/(
4
1
2
0
2
0
ω
πεπε
=
−
=
&
)/(cos)( 22
0
crt
E
m
Ne
td
e
−
−
= ω
ωω
A-field generated by the movement of electrons
2
042222
2
822
0
42
2
4
)(4
/)( E
cm
GReN
dvA
c
G
MM
e ωηωω
ω
ε
π
ω
+−
−=><=∆ ∫
ee
d
ηω
π
ωηωω
ωωω
ω 2)(
2
1
42222
2
≈
+−∫
2
0
2
822
0
4
8
/ E
RN
cm
Ge
MM
eηωε
π
−=∆
Mass reduction by the impressed electric field
mZe ee αω /2
=
Compared result with the Honda experiment
22
3/2 mce=Γ=η
2
2
13
1023.3/
t
V
RMM −
×−=∆
mmRmmtkVV 1,1,8 ===
1324
106,10 ×== eN ω
gM 28.1=∆
gM 63.09.0 ±=∆
(Abraham-Lorenz damping constant)
(dense hot plasma)
(Experiment)
Alternate external A-field
Mass shift of the dielectric material
Coupled with external forces
Net force generated
Mechanism of the Dynamical B-B effect
ZPF cutoff frequency shifted
A-fieldA-field
Capacitor
Dielectric material
2
2
13
1023.3/
t
V
RMM −
×−=∆
αM
dt
dM
v
dt
Mvd
F +==
)(
2
2
13
1023.3
t
V
t
Rv
M
M
t
v
∆
×=
∆
∆
−= −
α
Conservation of momentum
Acceleration of the moving body induced by
         the electric field
Factors to induce a weight loss of
the capacitor
• Increase the AC voltage impressed to the
capacitor, nonlinear increase of the
weight loss is produced.
• Increase the charge density of electric
current flowing through the capacitor,
the greater the weight loss
Electrogravitic propulsion
systems
Electrogravitic craft by Brown
Dielectric material Core mass
Positive pole
Negative pole
Electrode
(Brown disc airfoil)
Spark generated at the Brown’s experiment
Brown’s experimental results
• A large thrust was associated with spark.
A residual thrust existed without
sparking (1956)
• A DC voltage caused a thrust when
initially applied. The thrust would decay
within 60 seconds. (1928)
• The thrust varies with the time of
day(Both in vacuum and oil)
Electrogravitic craft (ARDA) by the JLN Labs
Electric field
2
0
2
822
0
4
8
E
vRN
cm
Ge
e τηωε
π
α
∆
=
Electrogravitic propulsion system
(Concept of the pulsed electric field plasma propulsion)
Thrust
[Features]
•Highly acceleration capability
•Low consumption of fuel
Inlet
(-)
(-) (-)
(+)v(+) (+) (+)(+) (+)(+)(+) (+)(+) (+)(+) (+)(+)(+)(+)
(+)v(+) (+) (+)(+) (+)
(+)
(+) (+)(+) (+) (+) (+)
(+)
(+)(+)(+)
(+)v
(+) (+)
Positively-charged
units
HV pulse generator
Electric field
Electric field
Ion source
Plasma cloud
Electric field
To leading edge
Power supply
Charged outer hull
Nozzle
Grid
R: Radius of plasma cloud
N: Plasma density
E0:Electric field
Conclusion
• From the theoretical analysis by the zero-point field
theory, it is considered that the origin of the
dynamical Biefeld-Brown effect might be attributed
to the interaction of zero-point vacuum fluctuations
with high potential electric field impressed to the
capacitor. This result suggests that the pulsed
electric field applied to the capacitor may produce
artificial gravity sufficient for practical application
to the space propulsion technology.
The End
INTERNATIONAL ACADEMY OF
ASTRONAUTICS
Missions to the outer solar system and
beyond
FIFTH IAA SYMPOSIUM ON REALISTIC
NEAR-TERM
ADVANCED SCIENTIFIC SPACE MISSIONS
Aosta, Italy, July 2-4, 2007
If you have any question, please send me a mail to
musha@cs.trdi.mod.go.jp
takaaki.musha@gmail.com

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Antigravity: Biefeld-Brown Effect / ZPF field

  • 1. Explanation of dynamical Biefeld-Brown Effect from the standpoint of ZPF field Takaaki Musha INTERNATIONAL ACADEMY OF ASTRONAUTICS Missions to the outer solar system and beyond FIFTH IAA SYMPOSIUM ON REALISTIC NEAR-TERM ADVANCED SCIENTIFIC SPACE MISSIONS Aosta, Italy, July 2-4, 2007
  • 2. Contents (1) Purpose (2) Outline of the dynamical B-B effect (3) Possibility of artificial gravity induced by dynamical electromagnetic field (4) Electrogravitic propulsion systems (5) Conclusion
  • 3. Purpose • To explain the weigh reduction at the experiment by applying alternate electric field to the capacitor conducted by the research group of the HONDA R&D Institute group from the standpoint of ZPF field in a space • To investigate the applicability of the dynamical Biefeld-Brown effect for the propulsion system
  • 4. Outline of the dynamical B-B effect • From the 1st of Feb. till the 1st of March in 1996, the research group of the HONDA R&D Institute conducted experiments to verify the B-B effect with an improved experimental device in 1996 to reject the influence of corona discharges and electric wind around the capacitor by setting the capacitor in the insulator oil contained within a metallic vessel. They found that the weight loss by the alternate electric field was greater than the static case .
  • 6. Electrical circuit for generating HV electric field
  • 7. Schematic diagram of the electric circuit 8kV AC pulse, f=50Hz,
  • 8. Histogram of weight losses observed at the experiment gM 63.09.0 ±=∆
  • 9. Forces generated by the ionic transfer of the momentum )/(/2 000 giqVmM ⋅=∆ By introducing experimental values, 1682pF, 8kV, and 50Hz, into the equation, the weight reduction due to ionic winds becomes 1.3×10-3g , which is negligible small compared with the experimental result. T.B.Bahder & C.Fazi
  • 10. EZEGZE rrg ⋅×−=⋅−≈ − εεπε 11 0 1062.84 )(002.0/1062.8 0 11 ggEWZM r =×=∆ − ε 22 ψµεψε SG d M GFg == (Musha: weak field approximation of general relativity theory) (Ivanov: Weyl-Majumdar-Papapetrou solutions of the general Relativity theory) Gravitational field generated by the B-B effect gM 63.09.0 ±=∆(Experiment)
  • 11. Possibility of artificial gravity induced by dynamical electromagnetic field
  • 12. 2 2 2 c m c π ωhΓ = ZPF field in a space ω π ω ωωρ d c d 32 3 2 )( h = Inertial mass is originated to the interaction of sub-elementary particles with the vacuum ZPF field Inertial mass generated by the ZPF field
  • 13. (M.B.King : Tapping the zero-point energy) A slight coherence of vacuum fluctuations due to the high potential electric field caused an alternation of inertial properties of the body with the ionic lattice of a rapidly spinning atom . (B.Haish, A.Rueda and H.E.Puthoff ) If one could somehow modify the vacuum medium then the mass of a particle or object in it would change according to the zero-point field theory.
  • 14. ><= 2 2 0 2 2 A cm e HA 2 3 0 2 2 cA cm e H ω π h =′ (A) Electrodynamic Hamiltonian by P.Milonni (B) Electromagnetic Hamiltonian corresponding Zero-point fields (B.Haisch, A.Rueda, H.E.Puthoff) Process to derive the anti-gravity equation
  • 15. A=0 No Electric field Electric field Impressed AA HH ′∆= Initial State 0=AH )( 0AAA HHH ′−′=′∆ Assumption to derive equation 0)( =′−∆ AA HH
  • 16. ><−=∆ 2 02 A c ω π ω h >< ω π =ωω∆−=∆ 2 2 0 0/2/ A c mm h Electrodynamic Hamiltonian AA HH ′∆= Equation of Mass Shift 2 2 2 c m c π ωhΓ =
  • 18. 2 042222 2 822 0 42 2 4 )(4 /)( E cm GReN dvA c G MM e ωηωω ω ε π ω +− −=><=∆ ∫ ee d ηω π ωηωω ωωω ω 2)( 2 1 42222 2 ≈ +−∫ 2 0 2 822 0 4 8 / E RN cm Ge MM eηωε π −=∆ Mass reduction by the impressed electric field mZe ee αω /2 =
  • 19. Compared result with the Honda experiment 22 3/2 mce=Γ=η 2 2 13 1023.3/ t V RMM − ×−=∆ mmRmmtkVV 1,1,8 === 1324 106,10 ×== eN ω gM 28.1=∆ gM 63.09.0 ±=∆ (Abraham-Lorenz damping constant) (dense hot plasma) (Experiment)
  • 20. Alternate external A-field Mass shift of the dielectric material Coupled with external forces Net force generated Mechanism of the Dynamical B-B effect ZPF cutoff frequency shifted A-fieldA-field Capacitor Dielectric material
  • 21. 2 2 13 1023.3/ t V RMM − ×−=∆ αM dt dM v dt Mvd F +== )( 2 2 13 1023.3 t V t Rv M M t v ∆ ×= ∆ ∆ −= − α Conservation of momentum Acceleration of the moving body induced by          the electric field
  • 22. Factors to induce a weight loss of the capacitor • Increase the AC voltage impressed to the capacitor, nonlinear increase of the weight loss is produced. • Increase the charge density of electric current flowing through the capacitor, the greater the weight loss
  • 24. Electrogravitic craft by Brown Dielectric material Core mass Positive pole Negative pole Electrode (Brown disc airfoil)
  • 25. Spark generated at the Brown’s experiment
  • 26. Brown’s experimental results • A large thrust was associated with spark. A residual thrust existed without sparking (1956) • A DC voltage caused a thrust when initially applied. The thrust would decay within 60 seconds. (1928) • The thrust varies with the time of day(Both in vacuum and oil)
  • 27. Electrogravitic craft (ARDA) by the JLN Labs Electric field
  • 28. 2 0 2 822 0 4 8 E vRN cm Ge e τηωε π α ∆ = Electrogravitic propulsion system (Concept of the pulsed electric field plasma propulsion) Thrust [Features] •Highly acceleration capability •Low consumption of fuel Inlet (-) (-) (-) (+)v(+) (+) (+)(+) (+)(+)(+) (+)(+) (+)(+) (+)(+)(+)(+) (+)v(+) (+) (+)(+) (+) (+) (+) (+)(+) (+) (+) (+) (+) (+)(+)(+) (+)v (+) (+) Positively-charged units HV pulse generator Electric field Electric field Ion source Plasma cloud Electric field To leading edge Power supply Charged outer hull Nozzle Grid R: Radius of plasma cloud N: Plasma density E0:Electric field
  • 29. Conclusion • From the theoretical analysis by the zero-point field theory, it is considered that the origin of the dynamical Biefeld-Brown effect might be attributed to the interaction of zero-point vacuum fluctuations with high potential electric field impressed to the capacitor. This result suggests that the pulsed electric field applied to the capacitor may produce artificial gravity sufficient for practical application to the space propulsion technology.
  • 30. The End INTERNATIONAL ACADEMY OF ASTRONAUTICS Missions to the outer solar system and beyond FIFTH IAA SYMPOSIUM ON REALISTIC NEAR-TERM ADVANCED SCIENTIFIC SPACE MISSIONS Aosta, Italy, July 2-4, 2007 If you have any question, please send me a mail to musha@cs.trdi.mod.go.jp takaaki.musha@gmail.com