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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 />

28

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