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Nembo Buldrini Aerospace Engineering FOTEC Forschungs- und Technologietransfer GmbH – Austria [email protected] Current pulse Coi l Ferrite block Final speed: v cl or v mf ? Possible Mach Effects in Bodies Accelerated by Non-Uniform Magnetic Fields

Nembo Buldrini Aerospace Engineering FOTEC Forschungs- und Technologietransfer GmbH – Austria [email protected] Nembo Buldrini Aerospace Engineering

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Page 1: Nembo Buldrini Aerospace Engineering FOTEC Forschungs- und Technologietransfer GmbH – Austria nevok.geo@yahoo.com Nembo Buldrini Aerospace Engineering

Nembo Buldrini

Aerospace EngineeringFOTEC Forschungs- und Technologietransfer GmbH – Austria

[email protected]

Nembo Buldrini

Aerospace EngineeringFOTEC Forschungs- und Technologietransfer GmbH – Austria

[email protected]

Current pulse

Coil

Ferrite block

Final speed:vcl or vmf ?

Possible Mach Effects in Bodies Accelerated by Non-Uniform Magnetic Fields

Possible Mach Effects in Bodies Accelerated by Non-Uniform Magnetic Fields

Page 2: Nembo Buldrini Aerospace Engineering FOTEC Forschungs- und Technologietransfer GmbH – Austria nevok.geo@yahoo.com Nembo Buldrini Aerospace Engineering

Mach Effects

The possibility to transiently alter the mass of a body (in figure AM, Active Mass) would enable the implementation of a unique

propulsion system, which wouldn’t require the ejection of propellant in order to produce thrust, thus overcoming the limits of rocket

propulsion.

The possibility to transiently alter the mass of a body (in figure AM, Active Mass) would enable the implementation of a unique

propulsion system, which wouldn’t require the ejection of propellant in order to produce thrust, thus overcoming the limits of rocket

propulsion.

Spacecraft AMAM

Page 3: Nembo Buldrini Aerospace Engineering FOTEC Forschungs- und Technologietransfer GmbH – Austria nevok.geo@yahoo.com Nembo Buldrini Aerospace Engineering

Mach Effects

Universe

In the so called “Mach effects”, this mass fluctuation would originate from a radiative transaction between the body itself

and the rest of the mass of the universe.

In the so called “Mach effects”, this mass fluctuation would originate from a radiative transaction between the body itself

and the rest of the mass of the universe.

Page 4: Nembo Buldrini Aerospace Engineering FOTEC Forschungs- und Technologietransfer GmbH – Austria nevok.geo@yahoo.com Nembo Buldrini Aerospace Engineering

Universe

Mach Effects

Any momentum gained by the body would be compensated by an equal amount of momentum gained by the rest of the universe, which will move by an infinitesimal

distance in the opposite direction, thus satisfying the momentum conservation law.One could say that, in a sense, the actual propellant is the universe itself.

Any momentum gained by the body would be compensated by an equal amount of momentum gained by the rest of the universe, which will move by an infinitesimal

distance in the opposite direction, thus satisfying the momentum conservation law.One could say that, in a sense, the actual propellant is the universe itself.

Page 5: Nembo Buldrini Aerospace Engineering FOTEC Forschungs- und Technologietransfer GmbH – Austria nevok.geo@yahoo.com Nembo Buldrini Aerospace Engineering

Mach Effects

2

2

0

0 )( t

Ektm

2

2

0

0 )( t

Ektm

2

0

2

20

20

2

20

0

11

4

1)(

t

E

ct

E

cGt

2

0

2

20

20

2

20

0

11

4

1)(

t

E

ct

E

cGt

this term is negligibleat low power

Integrating the equation over the volume of the body subjected to the energy variation, one gets the simple relation:

This is the final equation that describes the Mach effects:

Page 6: Nembo Buldrini Aerospace Engineering FOTEC Forschungs- und Technologietransfer GmbH – Austria nevok.geo@yahoo.com Nembo Buldrini Aerospace Engineering

Bulk Acceleration

In order for the Mach effects to manifest, it was noticed that the AM has to be subjected to a bulk acceleration (in addition to the internal energy variation). This fact comes from first principles of

the derivation itself. How much is the magnitude of such acceleration affecting the expression of mass fluctuation,

however, is not yet clear. At a first glance, the final equation:

seems mute about this, but Woodward will bring some insights about this issue during this forum...

In order for the Mach effects to manifest, it was noticed that the AM has to be subjected to a bulk acceleration (in addition to the internal energy variation). This fact comes from first principles of

the derivation itself. How much is the magnitude of such acceleration affecting the expression of mass fluctuation,

however, is not yet clear. At a first glance, the final equation:

seems mute about this, but Woodward will bring some insights about this issue during this forum...

2

2

0

0 )( t

Ektm

2

2

0

0 )( t

Ektm

Page 7: Nembo Buldrini Aerospace Engineering FOTEC Forschungs- und Technologietransfer GmbH – Austria nevok.geo@yahoo.com Nembo Buldrini Aerospace Engineering

Efficiency of Mach Effects

Given the last experimental results, the question why the magnitude of the recorded effect is so low compared to the one predicted by the theoretical model

remains open.As a first rough attempt to address this issue, it seems reasonable to insert into the mass fluctuation equation an efficiency parameter, which, for explanatory

reasons, will be split in two different components, η1 and η2

Given the last experimental results, the question why the magnitude of the recorded effect is so low compared to the one predicted by the theoretical model

remains open.As a first rough attempt to address this issue, it seems reasonable to insert into the mass fluctuation equation an efficiency parameter, which, for explanatory

reasons, will be split in two different components, η1 and η2

21

2

0

20 )( t

Ektm

The η1 parameter is the fraction of the energy injected into the active mass,

which is effectively contributing to a change of the internal energy.

The η2 parameter indicates the efficiency of the ME process itself, which could

depend on different factors (destructive interference, bulk acceleration magnitude,…)

The η1 parameter is the fraction of the energy injected into the active mass,

which is effectively contributing to a change of the internal energy.

The η2 parameter indicates the efficiency of the ME process itself, which could

depend on different factors (destructive interference, bulk acceleration magnitude,…)

Page 8: Nembo Buldrini Aerospace Engineering FOTEC Forschungs- und Technologietransfer GmbH – Austria nevok.geo@yahoo.com Nembo Buldrini Aerospace Engineering

Mach effect devices: past and present embodiments

~

Ballastmass

Actuator(piezoelectric material)

Active Mass:Capacitor’sdielectric

Power Supply

Thrust

~Capacitor

~Power Supply

Coil

Power Supply

MagneticFieldForce

ElectricField

Piezo-actuator type “Mach-Lorentz” device type

The experimental method used so far to investigate the existence of Mach effects is to subject capacitors to charge and discharge cycles while they are accelerated.

Two main types of devices have been build, which differs from the method used to accelerate the active mass (AM). In the piezo-actuator type, the capacitor is accelerated mechanically by a piezoelectric actuator; in the “Mach-Lorentz” device, the acceleration is provided by the Lorentz force, arising from the interaction of the electric field of the

capacitor with the B-field produced by an external coil

The experimental method used so far to investigate the existence of Mach effects is to subject capacitors to charge and discharge cycles while they are accelerated.

Two main types of devices have been build, which differs from the method used to accelerate the active mass (AM). In the piezo-actuator type, the capacitor is accelerated mechanically by a piezoelectric actuator; in the “Mach-Lorentz” device, the acceleration is provided by the Lorentz force, arising from the interaction of the electric field of the

capacitor with the B-field produced by an external coil

Page 9: Nembo Buldrini Aerospace Engineering FOTEC Forschungs- und Technologietransfer GmbH – Austria nevok.geo@yahoo.com Nembo Buldrini Aerospace Engineering

Mach effect devices: past and present embodiments

~

Ballastmass

Actuator(piezoelectric material)

Active Mass:Capacitor’sdielectric

Power Supply

Thrust

~Capacitor

~Power Supply

Coil

Power Supply

MagneticFieldForce

ElectricField

Piezo-actuator type “Mach-Lorentz” device type

The advantages of using a dielectric in a capacitor as active mass are: 1) Large internal energy variations are easily obtainable 2) Fast internal energy variation are easily obtainable

On the other hand, both device types have challenges to getting the dielectric properly accelerated. In the piezo-actuator type, for example, the reflection of shock waves on the surfaces could impede an uniform acceleration. In the “Mach-Lorentz” type, the

magnitude of the Lorentz force produced is usually rather small.

The advantages of using a dielectric in a capacitor as active mass are: 1) Large internal energy variations are easily obtainable 2) Fast internal energy variation are easily obtainable

On the other hand, both device types have challenges to getting the dielectric properly accelerated. In the piezo-actuator type, for example, the reflection of shock waves on the surfaces could impede an uniform acceleration. In the “Mach-Lorentz” type, the

magnitude of the Lorentz force produced is usually rather small.

Page 10: Nembo Buldrini Aerospace Engineering FOTEC Forschungs- und Technologietransfer GmbH – Austria nevok.geo@yahoo.com Nembo Buldrini Aerospace Engineering

In order to get easily both large internal energy variations and bulk accelerations, ferromagnetic materials could be used as active mass

Placing a ferromagnetic active mass in a pulsed non-uniform magnetic field, it will be subjected simultaneously to an internal

energy variation and a bulk acceleration.

If a mass fluctuation should take place, then the final speed should be higher than classically calculated

In order to get easily both large internal energy variations and bulk accelerations, ferromagnetic materials could be used as active mass

Placing a ferromagnetic active mass in a pulsed non-uniform magnetic field, it will be subjected simultaneously to an internal

energy variation and a bulk acceleration.

If a mass fluctuation should take place, then the final speed should be higher than classically calculated

A different experimental approach

AMAcceleration

Internal energy

variation

Page 11: Nembo Buldrini Aerospace Engineering FOTEC Forschungs- und Technologietransfer GmbH – Austria nevok.geo@yahoo.com Nembo Buldrini Aerospace Engineering

Let’s consider a simple device as the one here depicted…Let’s consider a simple device as the one here depicted…

A different experimental approach

A power supply (P/S) charges a capacitor (C) up to the desired voltage value. A switch (S) provides to transfer the energy of the

capacitor to a coil, in a form of a short and intense pulse. A cylinder of ferromagnetic material constitutes the active mass (AM) which is initially placed in the region where the B-field produced by the coil is divergent. This setup is very similar to what is usually referred to as

electromagnetic pulse accelerator, or coilgun.

A power supply (P/S) charges a capacitor (C) up to the desired voltage value. A switch (S) provides to transfer the energy of the

capacitor to a coil, in a form of a short and intense pulse. A cylinder of ferromagnetic material constitutes the active mass (AM) which is initially placed in the region where the B-field produced by the coil is divergent. This setup is very similar to what is usually referred to as

electromagnetic pulse accelerator, or coilgun.

P/S C

S

(see next slide)

D

Page 12: Nembo Buldrini Aerospace Engineering FOTEC Forschungs- und Technologietransfer GmbH – Austria nevok.geo@yahoo.com Nembo Buldrini Aerospace Engineering

In this phase the force is at its maximum

At the same time, the mass is at its minimum

During Phase 1 the current starts flowing into the coil and the B-field rises. The mass fluctuation in the AM (Active Mass) reaches its first positive peak.

But the magnetic force (F) acting on the AM is still low: the mass fluctuation here hardly affects the acceleration of the AM.

During Phase 1 the current starts flowing into the coil and the B-field rises. The mass fluctuation in the AM (Active Mass) reaches its first positive peak.

But the magnetic force (F) acting on the AM is still low: the mass fluctuation here hardly affects the acceleration of the AM.

Phase 2: maximum force acting on the AM, mass fluctuation reaches its negative peak. The AM acceleration is higher (blue trace) than in the “classical” case (yellow trace)

Phase 2: maximum force acting on the AM, mass fluctuation reaches its negative peak. The AM acceleration is higher (blue trace) than in the “classical” case (yellow trace)

Phase 3 is similar to Phase 1: no much deviation from the classical acceleration trace.Phase 3 is similar to Phase 1: no much deviation from the classical acceleration trace.

vcl

vmf

What happens during the discharge? (1)

Page 13: Nembo Buldrini Aerospace Engineering FOTEC Forschungs- und Technologietransfer GmbH – Austria nevok.geo@yahoo.com Nembo Buldrini Aerospace Engineering

What happens during the discharge? (2)

In this phase the force is at its maximum

At the same time, the mass is at its minimum

The size of the AM represents its mass

The displacementduring acceleration

is exaggerated

COIL

vcl

vmf

Page 14: Nembo Buldrini Aerospace Engineering FOTEC Forschungs- und Technologietransfer GmbH – Austria nevok.geo@yahoo.com Nembo Buldrini Aerospace Engineering

pAM

pAA

pAM > pAApAM = pAA = ptot = 0

pAM = Momentum of the active mass

pAA = Momentum of the accelerating apparatus (coil + p/s + chassis)

ptot = Total momentum

pAM = Momentum of the active mass

pAA = Momentum of the accelerating apparatus (coil + p/s + chassis)

ptot = Total momentum

ptot <> 0

A rudimentary propellantless propulsion device

Active MassActive Mass Accelerating apparatusAccelerating apparatus

The active mass is accelerated as described in the previous slides, but is then stopped inside the device. If Mach effects obtain, then

the final total momentum of the device should be <> 0.

The active mass is accelerated as described in the previous slides, but is then stopped inside the device. If Mach effects obtain, then

the final total momentum of the device should be <> 0.

Page 15: Nembo Buldrini Aerospace Engineering FOTEC Forschungs- und Technologietransfer GmbH – Austria nevok.geo@yahoo.com Nembo Buldrini Aerospace Engineering

A rudimentary propellantless propulsion device

Connecting the active mass to the device with a spring and repeating the discharge process, it is easy to imagine the following rudimentary propellantless propulsion device:

Connecting the active mass to the device with a spring and repeating the discharge process, it is easy to imagine the following rudimentary propellantless propulsion device:

Page 16: Nembo Buldrini Aerospace Engineering FOTEC Forschungs- und Technologietransfer GmbH – Austria nevok.geo@yahoo.com Nembo Buldrini Aerospace Engineering

A rudimentary propellantless propulsion device

It has been calculated that the same effect obtains if the waveform of the discharge is a damped sinusoid. In this case the the diode seen in the previous circuit will be not necessary and a LC resonant – more

efficient – system can be used.

It has been calculated that the same effect obtains if the waveform of the discharge is a damped sinusoid. In this case the the diode seen in the previous circuit will be not necessary and a LC resonant – more

efficient – system can be used.

— Current— Force— Mass fluctuation— Speed (classical)— Speed (with m-f)

Frequency and magnitude are not to scale!

Behaviour of previously seen quantities in case of damped sinusoid current discharge

Notice again that when the force (blue) is at a maximum, the mass fluctuation (red) is at a maximum negative. When the mass fluctuation is at a maximum positive, the force is zero.

Page 17: Nembo Buldrini Aerospace Engineering FOTEC Forschungs- und Technologietransfer GmbH – Austria nevok.geo@yahoo.com Nembo Buldrini Aerospace Engineering

Quantitative Analisys

In order to make a preliminary quantitative analysis, a system comprised of a coil and a ferrite cylinder (AM) has been modeled and

a finite element simulation has been carried out. This allowed to calculate the forces acting on the ferrite cylinder and the change in its

internal energy during the discharge.

In order to make a preliminary quantitative analysis, a system comprised of a coil and a ferrite cylinder (AM) has been modeled and

a finite element simulation has been carried out. This allowed to calculate the forces acting on the ferrite cylinder and the change in its

internal energy during the discharge.

Coil

Ferrite cylinder

Simulation parameters:

Coil: 100 turn, ext. 30mm int. 22mm, length 23mm.

Peak Current: 50A

Ferrite Cylinder: 20mm, h 15mm

Inductance (coil + partially inserted ferrite cylinder): 180uH

Simulation parameters:

Coil: 100 turn, ext. 30mm int. 22mm, length 23mm.

Peak Current: 50A

Ferrite Cylinder: 20mm, h 15mm

Inductance (coil + partially inserted ferrite cylinder): 180uH

Page 18: Nembo Buldrini Aerospace Engineering FOTEC Forschungs- und Technologietransfer GmbH – Austria nevok.geo@yahoo.com Nembo Buldrini Aerospace Engineering

Quantitative Analisys

With the system previously described and modeled, and the following parameters:

Natural frequency of the LC discharge circuit: 80 kHz

Efficiency parameter η1 = 0.1

Efficiency parameter η2 = 0.1

Pulse repetition rate: 130 Hz

It has been calculated that a thrust ofabout 130 µN shall be produced

The problem is: we have no idea of the real magnitude of η1 and η2 …

With the system previously described and modeled, and the following parameters:

Natural frequency of the LC discharge circuit: 80 kHz

Efficiency parameter η1 = 0.1

Efficiency parameter η2 = 0.1

Pulse repetition rate: 130 Hz

It has been calculated that a thrust ofabout 130 µN shall be produced

The problem is: we have no idea of the real magnitude of η1 and η2 …

Page 19: Nembo Buldrini Aerospace Engineering FOTEC Forschungs- und Technologietransfer GmbH – Austria nevok.geo@yahoo.com Nembo Buldrini Aerospace Engineering

0

2

4

6

8

10

12

14

0 5 10 15 20

Position of the AM [mm]

Forc

e [N

]

0.00E+00

2.00E-03

4.00E-03

6.00E-03

8.00E-03

1.00E-02

1.20E-02

1.40E-02

Ener

gy [J

]

Force [N]

Energy [J]

0

20

40

60

80

100

120

140

0 5 10 15 20

Position of the AM [mm]

Thru

st [u

N], F

orce

[N]

0.00E+00

2.00E-03

4.00E-03

6.00E-03

8.00E-03

1.00E-02

1.20E-02

1.40E-02

Ene

rgy

[J] Force [N]

Thrust [uN]

Energy [J]

Position = 0mm(max energy)

Position = 6.5mm(max thrust)

Position = 16.4mmPosition = 10.9mm(max force)

The position of the AM is critical in obtaining the maximum thrust. Placing the AM in the middle, maximum energy variation is obtained, but not force is exerted. Placing the AM in the point where max force is exerted, the energy variation is quite low. But there is a point between this two positions where thrust is maximized.

The position of the AM is critical in obtaining the maximum thrust. Placing the AM in the middle, maximum energy variation is obtained, but not force is exerted. Placing the AM in the point where max force is exerted, the energy variation is quite low. But there is a point between this two positions where thrust is maximized.

Max thrust

Quantitative AnalisysThrust Maximization

Page 20: Nembo Buldrini Aerospace Engineering FOTEC Forschungs- und Technologietransfer GmbH – Austria nevok.geo@yahoo.com Nembo Buldrini Aerospace Engineering

Material Selection

The ideal ferromagnetic material to be used as AM should have the following characteristics:

• High response to applied magnetic fields

• High internal resistance (reduced eddy currents)

• High internal energy storing capacity

A candidate material, because of the high energy storing capacity, could be Terfenol-D. It is a conducting material, so it will be preferably laminated in order to increase the internal resistance. Further material characterization will be necessary in order to assess the behaviour under pulsed magnetic fields.

The ideal ferromagnetic material to be used as AM should have the following characteristics:

• High response to applied magnetic fields

• High internal resistance (reduced eddy currents)

• High internal energy storing capacity

A candidate material, because of the high energy storing capacity, could be Terfenol-D. It is a conducting material, so it will be preferably laminated in order to increase the internal resistance. Further material characterization will be necessary in order to assess the behaviour under pulsed magnetic fields.

Page 21: Nembo Buldrini Aerospace Engineering FOTEC Forschungs- und Technologietransfer GmbH – Austria nevok.geo@yahoo.com Nembo Buldrini Aerospace Engineering

Conclusions and Recomendation

• A new system has been described, which can be used to investigate the existence of Mach effects

• The system relies on the interaction of ferromagnetic materials with pulsed non-uniform magnetic fields

• The same system could be used for the construction of a propellantless propulsion device

• A study aimed at finding and characterizing a suitable material to be used as active mass in the described device is required before starting the experimental activity

• An in depth analysis of the derivation of Mach effects, in order to understand the role of bulk acceleration and to help to estimate the magnitude to the described “efficiency” factors, is highly desirable and recommended.

• A new system has been described, which can be used to investigate the existence of Mach effects

• The system relies on the interaction of ferromagnetic materials with pulsed non-uniform magnetic fields

• The same system could be used for the construction of a propellantless propulsion device

• A study aimed at finding and characterizing a suitable material to be used as active mass in the described device is required before starting the experimental activity

• An in depth analysis of the derivation of Mach effects, in order to understand the role of bulk acceleration and to help to estimate the magnitude to the described “efficiency” factors, is highly desirable and recommended.

Page 22: Nembo Buldrini Aerospace Engineering FOTEC Forschungs- und Technologietransfer GmbH – Austria nevok.geo@yahoo.com Nembo Buldrini Aerospace Engineering

Current pulse

Coil

Ferrite block

Final speed:vcl or vmf ?

Nembo Buldrini

Aerospace EngineeringFOTEC Forschungs- und Technologietransfer GmbH – Austria

[email protected]

Nembo Buldrini

Aerospace EngineeringFOTEC Forschungs- und Technologietransfer GmbH – Austria

[email protected]

Possible Mach Effects in Bodies Accelerated by Non-Uniform Magnetic Fields

Possible Mach Effects in Bodies Accelerated by Non-Uniform Magnetic Fields

Thank you for your attention!Thank you for your attention!