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This paper presents the work of the LAPLACE Electromagnetism Research Group to build an experimental setup able to measure tiny forces that may appear in microwave cavities, in the context of EMDrive investigations. It is based on a commercial balance in the range of 0.1 mN sensitivity, a contactless feeding for more than 150 W RF power, and self calibrating device process. It requires a double cavity system in mirror configuration and is here experimented with frustum cavities, different from the NASA one [1]. The global setup can make force measurement and calibration in less than two seconds. Investigating two different cavities and various electromagnetic modes for the biggest, no force is reported while the 0.1 mN sensitivity is demonstrated.
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Progress In Electromagnetics Research M, Vol. 95, 45–52, 2020
Straightforward EMDrive Setup Using a Microwave Contactless
Transition: First Results on Frustum Cavities
Hugo Peyre*,J´erˆome Sokoloff, Olivier Pascal, Olivier Pigaglio, and Nathalie Raveu
Abstract—This paper presents the work of the LAPLACE Electromagnetism Research Group to build
an experimental setup able to measure tiny forces that may appear in microwave cavities, in the context
of EMDrive investigations. It is based on a commercial balance in the range of 0.1 mN sensitivity, a
contactless feeding for more than 150 W RF power, and self calibrating device process. It requires a
double cavity system in mirror configuration and is here experimented with frustum cavities, different
from the NASA one [1]. The global setup can make force measurement and calibration in less than two
seconds. Investigating two different cavities and various electromagnetic modes for the biggest, no force
is reported while the 0.1 mN sensitivity is demonstrated.
1. INTRODUCTION
The EMDrive concept is based on the idea that an asymmetric resonant cavity fed by microwave power
would produce a non-zero resulting force, hence violating the momentum conservation: Newton’s third
law. Although extremely weak, the existence of such a force may have huge consequences either in
fundamental physics or spatial propulsion. This is the reason that EMDrive research and EMDrive-like
force measurement are currently big challenges.
While McCulloch gives a possible theoretical explanation for the phenomenon [2], any EMDrive-
like force demonstration seems to be achievable only through experimental work. In 2016, White et al.,
from NASA, experimentally demonstrated the production of an EMDrive-like force by a frustum cavity.
This work constitutes the first peer-reviewed EMDrive paper [1] claiming an efficiency of 1.2 mN/kW for
their cavity. A couple of years later, a German research team (TU Dresden), led by Tajmar, replicated
the NASA’s experiment implementing others cavity configuration at different frequencies [3]. However,
they could not conclude on the existence of an EMDrive-like force because of the presence of parasitic
forces (thermal, electromagnetic, etc.). Although these two setups are very sensitive, the significant
mass hanged on a torsion pendulum causes inertia. It requires to wait for tens of seconds to record
data that have to be carefully post-processed to extract forces. The difficulty for calibrating, using
reference configurations or forces without modifying the measure environment, appears to be a key in
the challenge of having conclusive results.
The objective of this paper is to present the improved LAPLACE’s EMDrive experimental setup
and its first qualification tests with frustum cavities different from the NASA one [1]. This setup aims
to provide a straight and fast response, capable of testing a wide diversity of cavities or resonant modes.
It constitutes our contribution to the scientific community so that a larger number of research teams
can take part in the EMDrive scientific debate.
This article is the third in our publishing approach detailing the advances of the setup. The first
one focused on the development of this handy and affordable experimental setup [4]. It also revealed
results obtained with a set of cavities in “Shaker” original self-calibrating configuration. This mirror
Received 29 May 2020, Accepted 14 July 2020, Scheduled 7 August 2020
* Corresponding author: Hugo Peyre (peyre@laplace.univ-tlse.fr).
The authors are with the LAPLACE, CNRS, Universit´e de Toulouse, Toulouse, France.
46 Peyre et al.
configuration made it possible to discriminate the hypothetical force against the parasitic forces. The
conclusions were that no EMDrive-like force could be demonstrated above our sensitivity of 0.5 mN,
and that the thermal effect of the coaxial cable (feeding the cavities) was the main parasitic effect.
To eliminate this parasitic effect, a contactless microwave transition has next been designed.
Its characterization is presented in the second publication [5]. It was found to exhibit satisfying
electromagnetic performances and to transmit 150 W microwave power without affecting the force
measurement.
This third paper is now presenting the EMDrive-like force measurements performed thanks to
the assembly of the Shaker configuration together with the contactless microwave transition. The
elimination of the thermal parasitic effect of the cable makes it possible to imagine and implement a
straighter and faster experimental protocol which will radically improve the sensitivity of the setup
(Section 3.3). Moreover, in order to explore a wider diversity of resonant modes with higher quality
factor, another set of cavities has been realized (Section 2.2). In this study, a total of three modes will
be exploited in an attempt to produce forces, whose measurements are reported in Section 4.
2. EQUIPMENT
2.1. Experimental Setup
The description of the EMDrive experimental setup developed at the Plasma and Energy Conversion
Lab (LAPLACE, Toulouse, France) is detailed in [4]. A solid-state generator provides CW microwave
power up to 200 W. It can be accurately tuned from 2.43 to 2.47 GHz in order to properly feed a narrow
bandwidth resonant cavity. In addition, force measurement is performed with a precision balance
having a display accuracy of 10mg (0.1 mN). The whole setup is placed on a marble block to lower
environmental noise on the balance measurement (Figure 1) [4].
The RF power unit feeds resonant cavities in a Shaker configuration (Figure 1). This original
jbc
e
i
f
d
g
h
k
a
Figure 1. LAPLACE’s EMDrive experimental setup mounted (a) on a marble block. (b) Under the
Plexiglas enclosure, the operating part includes (c) the resonant cavities in Shaker configuration (here:
Big Shaker) placed (d) on the precision balance and (e) fed thanks to a contactless microwave transition;
(f) power probes collect the incident and reflected powers, and (g) standard weights are used for the
calibration processes of the balance. On the left of the enclosure, the monitoring part is made of (h) the
microwave source, (i) the powermeters, a computer for (j) real-time control and (k) the switch command
to select which cavity to feed.
Progress In Electromagnetics Research M, Vol. 95, 2020 47
configuration, proposed in [4], is an assembly of two identical cavities oriented in opposite directions. A
microwave switch selects which cavity is fed. If an EMDrive-like force exists, it then becomes possible to
almost instantaneously generate a thrust alternately directed downwards or upwards, without changing
any parasitic effect.
This configuration first aims at discriminating the parasitic effects by making a simple instant
difference between the two measured forces, and it secondly aims at measuring a relative force of twice
the EMDrive-like force at the instant of the cavity switch: it therefore doubles the setup sensitivity.
The main objective of this paper is to present the first EMDrive-like force measurements performed
thanks to the assembly of the Shaker configuration with our contactless microwave transition (Figure 1).
This transition has been designed to transmit high microwave power (150 W) using two separate
channels without affecting the force measurement [5]. Although a low gap difference has a minimal
influence on the electromagnetic performances of the contactless transition, an effort has been made to
maintain an air gap of 3 mm between the two parts of the transition, throughout the whole study.
2.2. Resonant Cavities
After the work described in [4] and [5] and for this third step of the EMDrive setup development at
the LAPLACE, we are using a simple design of frustum cavity (without any dielectric part) that
has been previously simulated and manufactured in two units. These cavities’ shape creates an
electromagnetic asymmetry (conical angle of 58) seemingly necessary to produce an EMDrive-like
force. Their dimensions have been set so that the fundamental mode can be excited in the frequency
band of the generator. Indeed, it is the simplest mode to drive and leads to the smallest dimensions
and therefore to the minimal weight. The inner diameter is 40 mm at the small end and 119.8 mm at
the large end. The axial height is 63.85mm. Further in this paper, these two cavities and the Shaker
configuration that they form will be called “Cavity 1A”, “Cavity 1B”, and “Small Shaker”.
In our first paper [4], no EMDrive-like force has been experienced above the setup minimum
sensitivity. Enhancing the electromagnetic energy stored in the cavity is one possible way to increase
this EMDrive-like force. At its resonant frequency, the stored energy ESis directly related to the
injected power Pinj and quality factor Q:
ES=Q
2πf0
Pinj (1)
The injected power Pinj is almost already maximized at about 150 W. It is equal to the power
delivered by the microwave generator (200 W), from which the losses in the microwave circuit (50 W,
1.2 dB) and the reflected power are subtracted. The latter (the reflected power) can often be neglected
at the resonance frequency since the cavity appears quite well matched then. At the end, the quality
factor Qtherefore needs to be improved to increase the stored energy ES.
In order to explore a greater diversity of electromagnetic configurations with higher quality factor,
our strategy has been to increase the cavities’ dimensions homothetically. As a result, we keep the same
cavity global shape, and it is only bigger. In this way, the higher order modes found in the frequency band
will exhibit higher quality factors and more complex fields distributions. After numerically studying
them, this approach leads to the realization of two bigger identical cavities, called “Cavity 2A” and
“Cavity 2B”. Their inner diameters are 8.56 cm at the small end and 25.52 cm at the large end, and
the heights are 13.57 cm. The Shaker configuration they form is called “Big Shaker”.
With these bigger cavities, several modes can be excited in the 2.43–2.47 GHz bandwidth. Only
two of them will be studied because of the chosen excitation probe. Due to the complexity of these two
modes, we cannot name them easily, so we will simply label them as modes “α”and“β”.
Table 1 gathers the main information about the cavities and the corresponding excited modes that
will be used for EMDrive-like force measurements. All of the electromagnetic performances have been
inferred from measurement with a Vector Network Analyzer (VNA).
For the big cavities, the asymmetry of the chosen excitation probe causes the cavities to have to
be fed slightly differently in order to be assembled in Shaker configuration. This results in variations in
resonance frequencies and matching levels, as shown in Table 1. It can also be checked that the quality
factors of the modes fed in these big cavities are greater than that of the fundamental mode. Those
48 Peyre et al.
Table 1. Excited mode characteristics based on VNA measurements (cavities only).
Configurations Small Shaker Big Shaker
Volume of one cavity (cm3)346.8 3350.1
Modes Fundamental mode Mode αMode β
Field E (simulations)
Prototyp es Cav. 1A Cav. 1B Cav. 2A Cav. 2B Cav. 2A Cav. 2B
Resonant frequency f (MHz) 2440.8 2440.8 2442.7 2442.6 2455.3 2454.5
Matching (dB) 24 21 24 15 47 38
Quality factor Q3,550 3,550 17,020 18,500 6,180 5,070
r
of mode αare still the highest with 17,020 and 18,500. Nevertheless, mode βis the best matched one
(47 dB and 38 dB).
3. METHODS
3.1. Measuring Setup Performances
Before each measurement run presented in Section 4, a video-recorded calibration routine is carried out
to check the sensitivity and the response time of the balance. As in reference [4], F1 class standard
weights are put on top of the Shaker configuration, placed on the balance. According to the balance
manufacturer’s given sensitivity, we first tested the 10 mg weight and found that it was almost never
seen. For this reason, the weight of 20 mg is preferred: it is always detected and is consistently measured
as 10 mg (i.e., a 10 mg error), as shown in Figure 2.
Compared to reference [4], the sampling period of the balance has been reduced from 80 to 20 ms.
Figure 2 also shows the unpredictable response time of the balance. In the worst case, this time reaches
1 second and will be further considered as the setup minimum time necessary to detect a force of that
magnitude (0.2mN).
-10
0
10
20
-0.5 0 0.5 1 1.5
Weighing (mg)
Acquisition time (s)
Weighing 1
Weighing 2
Weighing 3
Weighing 4
Weighing 5
Weighing 6
Figure 2. Calibration of the balance with the Big Shaker (Figure 1), mode α. 6 measurements of a
20 mg weight video synchronized to the instant of contact (orange cross).
Progress In Electromagnetics Research M, Vol. 95, 2020 49
3.2. Thermal Effects
During power-up, the presence of inner surface currents on the walls of the cavity generates ohmic losses.
The cavity then heats up, and the longer the power-up is, the hotter it gets. Convection is then created
in and around the cavity, and can be a source of parasitic force measurement [1, 6]. Fortunately, none
of these thermal induced parasitic forces was high enough to be detected by the balance, even after a
10-minutes long test power-up. No vacuum conditions is then required to avoid convection in our setup.
Another consequence of the rise in temperature of the cavity is its mechanical deformation. Due to
heating, the cavity increases in volume, and the resonance shifts towards the lower frequencies. At an
operating frequency chosen below the resonance, the cavity is sequentially unmatched, matched, and
unmatched again as its dimensions increase with time. With 150 W incident power and synchronizing
times at resonance, reflection results are shown on Figure 3.
-20 -15 -10 -5 0 5 10 15 20
-35
-30
-25
-20
-15
-10
-5
0
Time [s]
S11 [dB]
Cavity 1A
Cavity 1B
Cavity 2A (mode α)
Cavity 2B (mode α)
Cavity 2A (mode β)
Cavity 2B (mode β)
Figure 3. Thermal drift of the four cavities synchronized at their resonance. Incident power of 150 W.
Considering that the cavities are matched enough if the relative reflection is below 10 dB, it can
be noticed in Figure 3 that the thermal drifts of the mode αare the fastest ones (10 s for cav. 2B and 24 s
for cav. 2A). On the other hand, the thermal drifts of the small cavities are slower: 40 s approx. below
the 10 dB criteria. Those of the mode βare even the slowest: 80 seconds. This thermal phenomenon
depends on the mode ohmic losses, the volume and weight of the cavity, and the quality factor of the
excited mode.
These long thermal drift times (versus the weighing time) allow not to implement any resonance
frequency tracking circuit. This leads to a simpler and cheaper setup. Moreover, considering the 10 dB
matched criteria, the Shaker can be used during more than ten seconds while one is only required to
perform a single measurement, two seconds considering the two cavities of the Shaker. It is even more
advantageous with the Small Shaker.
3.3. Protocol
The elimination of the parasitic thermal effect of the coaxial cable, using the contactless feeding device
[5] together with almost instantaneous measurement and Shaker calibration, makes the new force
measurement protocol radically different from that of our reference [4] and others [1, 3]. No need to post-
process the measurement data to extract an EMDrive-like force: this improved setup is straightforward.
The measurement runs presented in Section 4 (see Figures 4, 5, and 6) are composed of a calibration
step immediately followed by a powering-up phase. The first operation (t5 s) is therefore a deposit
of a 20 mg standard weight on top of the Shaker configuration to make sure that the balance is able to
measure at least a 0.2mN force under these experimental conditions.
A few seconds later, an RF power of 200 W is delivered by the generator for a few tens of seconds
(20–30 s). This period is short enough to avoid any air convection interfering the force measurement
50 Peyre et al.
(Section 3.2). Ultimately, an average of about 150 W reaches the input of the cavities, and power
measurements prove that the cavities remain matched.
To combine these two operations, a specific structure has been set up in the Plexiglas enclosure
to be able to perform the weight calibration without opening and closing the doors. There is no need
for anyone to operate within the compound, and this allows the consistency of the force measurement
between the two phases.
During the powering-up phase, almost instant switching between the two cavities is performed
thanks to the microwave switch. Indeed, the commutation time is below the millisecond which remains
much lower than the sampling period (20 ms) and the response time of the balance (1 s). The duration
and the choice of the cavity feeding are arbitrarily chosen and are actually in the range of 2 to 6 seconds.
It remains higher than the response time of the balance.
During these periods, the feeding frequency is not changed. A preliminary process is therefore
necessary to match the two cavities in the same mode, at the same resonance frequency. For this
purpose, the thermal drift phenomenon is taken advantage of. Indeed, before each measurement run,
both cavities are more or less fed (and so heated) to adjust their resonance frequencies so that they
become equal.
To summarize, the sensitivity of the precision balance is 0.2 mN, under the experimental conditions.
Now, since both cavities are well matched each time they are fed, we can assume that they could produce
two opposite EMDrive-like forces. We can then easily conclude that a relative thrust of twice this force
is measurable at the instant of the switch (with a sensitivity of 0.2 mN). In that way, we can state that
the global sensitivity of the whole setup is divided by 2 and the ability to detect an EMDrive-like force
reduced to 0.1 mN.
4. RESULTS
In this section, we present the first EMDrive-like force measurement results using the Shaker
configuration in combination with the contactless transition.
For each of the three tested configurations, the measurement run includes a calibration step and
a power-up phase, as described in the previous protocol (Section 3.3). On the upper part of the
chronograms, the weighing data are displayed in blue (mg scale on the left and mN scale on the right
assuming g10 m ·s2). Below, the power curves are plotted showing the incident power in orange
and the reflected power in brown (W scale on the right).
The first configuration concerns the fundamental mode fed in the cavities of the Small Shaker (see
Figure 4). The calibration step is started at t3 s, and the power is applied at t7 s, beginning with
cavity 1A. Then, several cavity switches are sequentially operated.
0
25
50
75
100
125
150
175
200
225
250
10
0
10
20
0 5 10 15 20 25 30
Power (W)
Weighing (mg)
Acquisition time (s)
Weighing (mg)
Incident power (W)!
Reflected power (W)!
Cavity A Cavity B B ABB
AA
AB
Force variation (mN)
0.1
0.1
0
Weight deposit
Acquisition time(s)
5
Figure 4. First experimental run chronogram gathering all the collected measurements. Small Shaker
configuration (Cavities 1A & 1B), Fundamental mode. 20 mg calibration and then 200 W RF power at
2440 MHz.
Progress In Electromagnetics Research M, Vol. 95, 2020 51
0
25
50
75
100
125
150
175
200
225
250
-10
0
10
20
0 5 10 15 20 25 30 35 40 45
Power (W)
Weighing (mg)
Acquisition time (s)
Weighing (mg)
Incident power (W)
Reflected power (W)
Cavity B Cavity A BABBBA AAA
B
0.1
-0.1
0
Force variation (mN)
Weight deposit
Figure 5. Second experimental run chronogram gathering all the collected measurements. Big Shaker
configuration (Cavities 2A & 2B), Mode α. 20 mg calibration and then 200 W RF power at 2442.2 MHz.
0
25
50
75
100
125
150
175
200
225
250
-80
-70
-60
-50
-40
-30
-20
-10
0
10
20
0 5 10 15 20 25 30
Power (W)
Weighing (mg)
Acquisition time (s)
Weighing (mg)
Incident power (W)
Reflected power (W)
Weight deposit
Cavity B
Cavity A AB
AAB
0.1
-0.1
0
Force variation (mN)
Figure 6. Third experimental run chronogram gathering all the collected measurements. Big Shaker
configuration (Cavities 2A & 2B), Mode β. 20 mg calibration and then 200 W RF power at 2454.2 MHz.
It can clearly be seen in Figure 4 that the measured weight remains unchanged after the calibration
step. It suggests that no EMDrive-like force appears when the cavities are alternately fed with microwave
power. A global conclusion will take place at the end of the three runs.
The second measurement run involves the Big Shaker and the mode α, with the highest Q(see
Figure 5). As usual, the 20 mg weight is applied, at t4 s, and the power-up phase at t10 s. It
begins with cavity 2B. On the reflected power curve, the cavity switch can be observed more clearly
here thanks to the different matchings of the two cavities.
Finally, the third run is performed thanks to the Big Shaker configuration and the mode β,which
is the best matched one (≈−40 dB) (see Figure 6). The calibration step starts here at t5s, and
the power is applied at t10 s. It begins with cavity 2A. It can be seen in Figure 6 that the cavity
switches are barely noticeable because of the very good matching of both cavities.
During all these three runs, the 20 mg weight is measured at 10 mg, and then no weight variation
is recorded, even on the last balance digit. Therefore, it can be concluded that no force greater than
0.2 mN is detected by the balance when microwave power is applied. Remembering that at the cavity
switches events, the relative force is theoretically doubled, it can be said that no EMDrive-like force
above 0.1 mN has been measured with the LAPLACE’s EMDrive experimental setup for these three
configurations.
52 Peyre et al.
5. CONCLUSION
This experimental setup allows very fast and straightforward measurements of EMDrive-like forces.
No parasitic effect impacts the measurement thanks to the addition of the contactless microwave
transition, which can transmit more than 150 W power to the cavities. Only the thermal drift of the
resonance still needs to be considered in initializing our protocols.
The considered response time of this setup can be overestimated to 2 seconds. It is limited only by
the balance response time and the low inertia of the Shaker configuration. The external power supply
combined with the contactless transition minimizes the mass of the device under test. The resulting
elimination of the thermal effect of the previous feeding cable makes it possible to consider much faster
measurement protocols.
Moreover, the Shaker configuration plays an important role here by creating a double prospective
force at the cavity switch events. The creation of easy reading chronograms integrating the calibration
step allows a quick and direct interpretation of the measurement results.
We have to emphasize that no EMDrive-like force has been detected above 0.1 mN so far.
The forthcoming use of a new and more sensitive balance (display accuracy of 1 mg, 0.01 mN) will
be a significant improvement for the sensitivity of our setup. The final step of our EMDrive study will be
the replication of the NASA’s cavities [1]. Until now, no EMDrive-like force has been detected with our
setup. Perhaps this is because our cavities do not exhibit the same efficiency as NASA’s (1.2 mN/kW).
If they could, the resulting force would be 0.18 mN and would have been detected by our setup. The
implementation of the NASA-like cavities is going on, and we will soon be able to compare our results
with the other research teams [1, 3].
ACKNOWLEDGMENT
All the authors would like to thank both CNES (French National Centre for Space Studies) and AID
(French Innovation and Defense Agency) for funding Hugo Peyre’s work.
REFERENCES
1. White,H.,P.March,J.Lawrence,J.Vera,A.Sylvester,D.Brady,andP.Bailey,“Measurement
of impulsive thrust from a closed radio-frequency cavity in vacuum,” Journal of Propulsion and
Power, Vol. 33, 830841, Jul 2017.
2. McCulloch, M. E., “Propellant-less propulsion from quantized inertia,” Journal of Space
Exploration, Vol. 7, 1–7, 2018.
3. K¨oßling, M., M. Monette, M. Weikert, and M. Tajmar, “The spacedrive project — Thrust balance
development and new measurements of the mach-effect and emdrive thrusters,Acta Astronautica,
Vol. 161, 139152, Aug. 2019.
4. Sokoloff, J., O. Pascal, O. Pigaglio, N. Raveu, and H. Peyre, “Proposal of a handy setup for
discriminating parasitic effects for the measurement of impulsive thrust from a microwave cavity,”
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5. Peyre, H., O. Pascal, J. Sokoloff, K. Elis, O. Pigaglio, and N. Raveu, “High power transmission
using contactless microwave transition on an emdrive setup,” Progress In Electromagnetics Research
Letters, Vol. 90, 15–20, 2020.
6. McDonald, M. S., M. W. Nurnberger, and L. T. Williams, “Preparations for thrust measurement
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... For our study, at the LAPLACE Plasma and Energy Conversion Laboratory, we developed a basic setup producing almost instantaneous calibrations and results [4][5][6]. In this paper, we present how we replicated two NASA-like cavities in order to exploit the same electromagnetic configuration, or resonant mode. ...
... The main parts of the LAPLACE's EMDrive experimental setup, depicted in Figure 5, are extensively described in our previous papers [4][5][6]. Actually, the setup configuration is almost identical to that established in reference [6]: the cavities in Shaker configuration, positioned on the precision balance, are fed by the RF power unit through the contactless microwave transition. The two quasi-identical copper cavities are assembled and oriented in opposite directions. ...
... The main parts of the LAPLACE's EMDrive experimental setup, depicted in Figure 5, are extensively described in our previous papers [4][5][6]. Actually, the setup configuration is almost identical to that established in reference [6]: the cavities in Shaker configuration, positioned on the precision balance, are fed by the RF power unit through the contactless microwave transition. The two quasi-identical copper cavities are assembled and oriented in opposite directions. ...
... Due to the high weight and stiff coaxial cable from the amplifier, no force was measured for a thruster operating with 2.45 GHz, a Q factor of 3550, and a power of 140 W within their measurement resolution of 0.5 mN. Shortly afterward, an update was published by Peyre et al. [25] with a contactless microwave connection and an increased Q factor of up to 18,500, where no force was measured down to 0.1 mN for a power of 150 W fed into the cavity. Recently, this test was repeated with a cavity including a dielectric insert with a Q factor of 7,000 at a power of 160 W with the same mode (TM212) as White et al. [3], and again, no force was measured [26]. ...
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This paper details the work of the LAPLACE Electromagnetism Research Group to develop an original measuring setup dedicated to the detection of an EMDrive like force. Recent peer-reviewed experimental results were obtained using similar setups based on a torsion pendulum combined with an optical sensor. These very accurate measurement setups are appropriate for measuring such an extremely weak force. They also appear costly, which may discourage other research teams from working on this topic. Our main goal is then to provide an alternative configuration, based on a commercial precision balance, in order to build a measuring setup more affordable, handy, and accurate enough to measure an EMDrive like force. Our experimental system is capable of feeding a truncated cone shaped 2.45 GHz resonant cavity with power up to 140 W. To calibrate the EMDrive force and avoid false positive thrusts, an original setup has been proposed and evaluated. It allows us to really consider that the parasitic effects do not alter the hypothetical force measurement by the use of force direction switching during the measurement.
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Forces claimed by potential propellantless propulsion systems like the Mach-Effect-Thruster or the EMDrive are in the μN or even sub-μN range. In this paper, an automated thrust balance design capable of measuring forces of 100 nN for devices with a maximum mass of 10 kg is described to test these claims. The torsion balance features an electromagnetic calibration method, adjustable magnetic damping and tilt control as well as electromagnetic shielding. All onboard electronics can be controlled wirelessly via an infrared module for serial communication. Power is supplied to the balance using three separate liquid metal feedthroughs: one for voltages up to 500 V and frequencies up to 200 kHz, one for high voltage up to 30 kV DC or AC, and one for high frequency signals up to 3 GHz. The device can be rotated by 180° to measure three different thrust directions without breaking the vacuum and changing the setup in order to gain confidence and refute e.g. thermal drifts. The whole balance is controlled via a script language implemented in LabVIEW. We tested Mach-Effect-Thrusters provided by Woodward and our self-built model exploring higher frequencies and mixed-signals that are believed to create significantly higher forces. Also a magnetostrictive version was built and tested. For the EMDrive, several different frequencies and setups (with/without dielectric insert, flat/spherical end caps) were tested. Results of the tests performed between August and September 2018 are presented, but no final conclusions can be drawn.
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A vacuum test campaign evaluating the impulsive thrust performance of a tapered radio-frequency test article excited in the transverse magnitude 212 mode at 1937 MHz has been completed. The test campaign consisted of a forward thrust phase and reverse thrust phase at less than 8×10−6 torr vacuum with power scans at 40, 60, and 80 W. The test campaign included a null thrust test effort to identify any mundane sources of impulsive thrust; however, none were identified. Thrust data from forward, reverse, and null suggested that the system was consistently performing with a thrust-to-power ratio of 1.2±0.1 mN/kW.
Propellant-less propulsion from quantized inertia
  • M E Mcculloch
McCulloch, M. E., "Propellant-less propulsion from quantized inertia," Journal of Space Exploration, Vol. 7, 1-7, 2018.
Preparations for thrust measurement and error discussion of the impulse resonant microwave cavity
  • M S Mcdonald
  • M W Nurnberger
  • L T Williams
McDonald, M. S., M. W. Nurnberger, and L. T. Williams, "Preparations for thrust measurement and error discussion of the impulse resonant microwave cavity," Journal of the British Interplanetary Society, Vol. 70, 415-424, 2017.