12.12.2012 Views

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

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

S<strong>in</strong>ce the equation has the same form as Eq. (3.1), it will also have the<br />

same solutions <strong>and</strong> as the <strong>in</strong>itial conditions are identical, the formulas<br />

for the resonant field amplitude <strong>and</strong> the impact velocity will be identical.<br />

However, it should be noted that <strong>in</strong>stead <strong>of</strong> νc one will have ν <strong>and</strong> v0<br />

should be replaced by u0. An important difference is that the velocity<br />

<strong>in</strong> the previous model was only directed <strong>in</strong> the x-direction, but now<br />

there is also a thermal velocity component, vt, i.e. the total velocity<br />

is v = u + vt. With these new designations, the expressions for the<br />

resonant field amplitude <strong>and</strong> the impact velocity become:<br />

E0 =<br />

m<br />

e (ω2 + ν2 )(d + u0<br />

ν (Φ − 1))<br />

(1 + Φ)s<strong>in</strong> α + ((1 − Φ) ω<br />

ν<br />

2ν + ω )cos α<br />

(3.11)<br />

uimpact = u0Φ + Λ(1 + Φ)(ω cos α − ν s<strong>in</strong>α) (3.12)<br />

where Φ = exp (−Nπν/ω) has been <strong>in</strong>troduced for simplicity. Λ is given<br />

by Eq. (3.4) as before, but νc should be replaced by ν.<br />

In order to construct the multipactor boundaries, the same approach<br />

as <strong>in</strong> the simple model case is taken <strong>and</strong> an expression for the resonant<br />

phase is obta<strong>in</strong>ed by comb<strong>in</strong><strong>in</strong>g Eqs. (3.11) <strong>and</strong> (3.12), which yields,<br />

tan α = ω2 [ρΦ + χ] + 2ν 2 (Φu0 − uimpact)<br />

(dν + uimpact − u0)νω(1 + Φ)<br />

(3.13)<br />

where ρ = dν + uimpact + u0 <strong>and</strong> χ = dν − uimpact − u0 have been<br />

used for convenience. The reason why the expression looks somewhat<br />

different from Eq. (3.7) is that the constant <strong>in</strong>itial velocity approach has<br />

been used <strong>in</strong>stead <strong>of</strong> the assumption <strong>of</strong> a constant ratio between impact<br />

<strong>and</strong> <strong>in</strong>itial velocities. This will also affect the expression for the phase<br />

stability factor, which <strong>in</strong> this case becomes<br />

G = (Φ − 1)(ν2 + ω 2 )s<strong>in</strong> αΛ − Φνu0<br />

ν((1 + Φ)(ν s<strong>in</strong> α − ω cos α)Λ − Φu0)<br />

(3.14)<br />

So far, the differences between the simple <strong>and</strong> the more advanced<br />

model are fairly trivial. However, the parameters used (νc <strong>and</strong> νiz)<br />

are not constants, they depend to a great extent on the total electron<br />

velocity, which is the vector sum <strong>of</strong> the drift <strong>and</strong> thermal velocities. The<br />

thermal velocity will have a r<strong>and</strong>om direction <strong>and</strong> therefore the average<br />

total velocity will be equal to the drift velocity. However, the total<br />

(average) energy, ɛ, will still depend on both velocities <strong>and</strong> it becomes,<br />

ɛ = mv2<br />

2<br />

= m<br />

2 (u2 + 〈vt 2 〉) (3.15)<br />

45

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!