Multipactor in Low Pressure Gas and in ... - of Richard Udiljak
Multipactor in Low Pressure Gas and in ... - of Richard Udiljak
Multipactor in Low Pressure Gas and in ... - of Richard Udiljak
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where kn is a factor determ<strong>in</strong><strong>in</strong>g the frequency spac<strong>in</strong>g<br />
kn = fn/f0 − 1, n = 0,1,...,N − 1 , (2.27)<br />
f0 is the lowest carrier frequency <strong>and</strong> ω0 = 2πf0. When assess<strong>in</strong>g the<br />
worst case scenario from the multipactor po<strong>in</strong>t <strong>of</strong> view, it is important<br />
to study a whole envelope period. For arbitrarily spaced frequencies, the<br />
envelope period, T, can be found by solv<strong>in</strong>g the follow<strong>in</strong>g Diophant<strong>in</strong>e<br />
systems <strong>of</strong> equations:<br />
T = ni<br />
, ni ∈ N i = 1,2,...,N − 1 (2.28)<br />
∆fi<br />
where N is the number <strong>of</strong> carriers, f0 is the signal with the lowest frequency<br />
<strong>and</strong> ∆fi = fi − f0. The envelope period will be the solution<br />
with the smallest possible <strong>in</strong>tegers. For equally spaced carriers, the solution<br />
becomes n1 = 1, n2 = 2,...,nN−1 = N − 1, which is implies that<br />
T = 1/∆f, like before.<br />
When study<strong>in</strong>g multicarrier multipactor it is common to make certa<strong>in</strong><br />
simplifications that will allow us<strong>in</strong>g s<strong>in</strong>gle carrier methodology to<br />
asses also the multicarrier case, e.g. the mean frequency <strong>of</strong> all the carriers<br />
is used as the design frequency. Thus, most <strong>of</strong> what has been said<br />
about s<strong>in</strong>gle carrier multipactor will then be valid also for the multiple<br />
signals case.<br />
2.3 Design guidel<strong>in</strong>es<br />
From an <strong>in</strong>dustrial po<strong>in</strong>t <strong>of</strong> view it is important not only to underst<strong>and</strong><br />
the physics <strong>of</strong> multipactor, but also how the theoretical <strong>and</strong> experimental<br />
results should be applied when mak<strong>in</strong>g multipactor-free microwave<br />
hardware designs. In Europe, most space hardware designers follow the<br />
st<strong>and</strong>ard issued by ESA [50]. This st<strong>and</strong>ard <strong>in</strong>cludes both the s<strong>in</strong>gle<br />
<strong>and</strong> the multicarrier cases, but for the latter it is stated that the design<br />
guidel<strong>in</strong>es are only recommendations. Most research support these<br />
recommendations, but not enough tests have been performed to verify<br />
the theoretical f<strong>in</strong>d<strong>in</strong>gs. When us<strong>in</strong>g the st<strong>and</strong>ard it is important to be<br />
aware <strong>of</strong> the fact that it is primarily based on the parallel-plate model<br />
with a uniform electric field. Design with respect to this approach for<br />
other geometries is normally a conservative <strong>and</strong> safe way. However, <strong>in</strong><br />
many common microwave structures, the geometry is such that losses<br />
<strong>of</strong> electrons is much higher than <strong>in</strong> the parallel-plate case. Thus the<br />
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