EE 499 · Satellite Technologies

Week 5

We Have a Spacecraft in Orbit. Now How Do We Talk to It?

Four weeks of orbital mechanics told us where the spacecraft is. This week we build the link to it — and every step is an engineering decision that forces the next one.

By the end: you should be able to explain why the link frequency must sit far above the ionospheric limit, why antenna directivity pushes it higher still, why that lands satellite communications in the microwave bands, why microwave power is carried in waveguide rather than wire, and how to size a rectangular waveguide for a given operating frequency.

Primary source: the original lecture notes, Topic 3 — sections 1.1, 1.2, 1.3, 1.3.1 and 1.3.2.

01 — The link problem

The link we have to build

An earth station transmitting to a satellite A dish antenna standing on the curved surface of the Earth radiates a narrow beam up and to the right, across the space channel, to a satellite in orbit. earth station satellite the space channel — tens of thousands of kilometres of nothing a narrow beam, not a glow in every direction
Weeks 1 to 4 fixed the geometry of this picture. Week 5 is about the arrow.
  1. transmitter
  2. transmission structure
  3. antenna
  4. space channel
  5. satellite

01 — The link problem

One decision forces the next

This lecture is a single chain of engineering decisions. Nothing in it is chosen for mathematical convenience — each step is forced by the one before it, and we will walk the chain from the left.

  1. pick a frequency
  2. cross the ionosphere
  3. get directivity
  4. so: microwaves
  5. feed the antenna
  6. so: waveguide
  7. modes & cutoff

Part 1 — the first decision

What frequency should we use?

Before power, before modulation, before antennas: a carrier frequency. It is the one choice that constrains everything else, and the first thing that constrains it is what the signal has to travel through.

02 — Choosing a frequency

What the signal has to get through

Layers between an earth station and a satellite Stacked atmospheric layers above the ground: troposphere to about 12 km, stratosphere to about 50 km, mesosphere to about 80 km, and the ionosphere from about 80 km to about 300 km, above which satellites orbit in free space. free space — satellites orbit here IONOSPHERE — free electrons and ions mesosphere stratosphere troposphere — weather, rain, water vapour solar ultraviolet and X-rays strip electrons from the thin gas here this is the layer that decides our lowest usable frequency ground ~300 km ~80 km ~50 km ~12 km 0 km altitudes are those given in the notes; the vertical scale is not linear
The ionosphere extends roughly from \(80\ \text{km}\) to \(300\ \text{km}\), and its detailed behaviour changes from day to night and from season to season.

03 — The ionosphere

Sunlight makes a conductor out of thin air

High in the atmosphere the gas is extremely thin and completely exposed to the Sun. Ultraviolet and X-ray photons arriving there carry enough energy to knock electrons off the atoms and molecules they strike:

  1. solar radiation
  2. electrons stripped from atoms
  3. free electrons & ions
  4. a plasma
  5. radio propagation changes

The result is a region containing free charge. Everywhere else on the path the wave simply travels; here it meets charges that can move in response to its own electric field, and a medium that responds is a medium that changes how the wave behaves.

Because the energy supply is sunlight, the layer is not constant. It is stronger by day than by night and varies with season and with solar activity — which is exactly what the notes record.

03 — The ionosphere

Reflected, or passed through?

One threshold decides it, and it is set by how many free electrons there are. The notes give it as:

\[f_{\text{critical}}=9\sqrt{N_{\max}}\]

\(N_{\max}\) is the maximum electron density in electrons per cubic metre; \(f_{\text{critical}}\) comes out in hertz. This threshold is the layer's plasma frequency.

Below \(f_{\text{critical}}\) the electrons can follow the wave's field, the layer acts as a reflector and the wave is turned back. Above it the field reverses faster than the electrons can respond, and the wave passes through.

From the original lecture notes · Topic 3, p. 3 →

03 — The ionosphere

From electron density to a frequency floor

  1. A known figure for the maximum electron density is \(N_{\max}=10^{6}\ \text{electron/cm}^{3}\). Convert to SI first: \(1\ \text{cm}^{3}=10^{-6}\ \text{m}^{3}\), so \(N_{\max}=10^{12}\ \text{electron/m}^{3}\).
  2. Substitute: \(f_{\text{critical}}=9\sqrt{10^{12}}=9\times10^{6}\ \text{Hz}=9\ \text{MHz}\).
  3. That figure is for a wave arriving perpendicular to the layer. Arriving at an angle makes reflection easier, and raises the limit by a factor of about three to four.
  4. \(9\ \text{MHz}\times(3\ \text{to}\ 4)\approx30\ \text{MHz}\) — the highest frequency that can practically be reflected by the ionosphere.

From the original lecture notes · Topic 3, p. 4 →

03 — The ionosphere

The same layer, two completely different outcomes

Sky-wave propagation compared with a satellite path A low-frequency ray leaves a transmitter, reflects from the ionosphere and returns to a distant receiver on the ground. A higher-frequency ray from a second station passes straight through the ionosphere to a satellite. IONOSPHERE reflected f below f-critical: the electrons follow the field, so the layer acts as a mirror passes through f well above f-critical: the field reverses faster than the electrons can respond HF transmitter distant receiver earth station satellite
The left-hand path is how long-distance short-wave radio works. Our link needs the right-hand one, so the notes require a frequency well above the limit — not merely above it, because \(f_{\text{critical}}\) itself moves with day, season and solar activity.

03 — The ionosphere

Check yourself

1 · A 10 MHz uplink

An engineer proposes a \(10\ \text{MHz}\) uplink to a geostationary satellite. What is the decisive objection?

Part 2 — the second decision

Is getting through the ionosphere enough?

No. A frequency above \(30\ \text{MHz}\) will leave the atmosphere — and then spread its power over the whole sky. The spacecraft intercepts almost none of it.

04 — Directivity

We do not want to radiate in every direction

A geostationary satellite is a small target \(36{,}000\ \text{km}\) away. An antenna that radiates equally in all directions sends almost all of its power somewhere the spacecraft is not, and interferes with everyone else while doing it.

What we actually need is directivity: the ability to concentrate radiated energy into a narrow cone aimed at the spacecraft. That requirement, not the ionosphere, is what pushes the frequency much higher than \(30\ \text{MHz}\).

From the original lecture notes · Topic 3, p. 6 →

04 — Directivity

The same dish, at two different frequencies

Beamwidth of one antenna aperture at two frequencies The same physical dish is shown twice. At 3 GHz, where the wavelength is 100 mm, it radiates a broad beam. At 12 GHz, where the wavelength is 25 mm, the identical dish radiates a much narrower beam. D f = 3 GHz λ = 100 mm  ·  a 1 m dish is 10 wavelengths across broad beam D f = 12 GHz λ = 25 mm  ·  the same dish is 40 wavelengths across narrow beam the metal did not change — only the wavelength did
Four times the frequency is a quarter of the wavelength, which makes the same dish four times larger electrically: roughly a quarter of the beamwidth and about sixteen times the directivity.

04 — Directivity

Why shorter waves buy directivity

For an aperture antenna — a dish, a horn, an array — directivity scales with the aperture area measured in square wavelengths:

\[D\;\propto\;\frac{A}{\lambda^{2}},\qquad\quad \lambda=\frac{c}{f}\]

So for a fixed physical aperture \(A\), doubling the frequency halves \(\lambda\) and quadruples the directivity.

That is the whole argument. The dish on the roof is a fixed number of metres across, and we cannot keep making it bigger. The only remaining way to make it electrically larger is to shorten the wavelength — which means raising the frequency.

Antennas are a topic of their own later in the course; here we need only the scaling, not the full aperture theory.

04 — Directivity

Check yourself

2 · From 3 GHz to 12 GHz

A fixed \(1\ \text{m}\) dish is moved from \(3\ \text{GHz}\) to \(12\ \text{GHz}\). What happens to the wavelength, and what does the dish gain?

05 — Into the microwave region

The physics pushes us toward microwaves

Three independent requirements, all pointing the same way:

Get through the ionosphere

A floor of roughly \(30\ \text{MHz}\), and we want to be well clear of it because the threshold moves.

Get directivity

The aperture must be many wavelengths across, so \(\lambda\) must be small.

Keep the antenna buildable

The dish has to fit on a roof, a ship or a spacecraft, so we cannot buy electrical size with metres.

  1. all three constraints
  2. short wavelength
  3. GHz — the microwave region

A fourth, historical reason from the notes: by the end of the 1930s radio and television already occupied the MF, HF, VHF and UHF bands, so satellite systems in the 1950s had to be placed above them.

06 — Satellite bands

Where the satellite bands sit

Now the band chart means something. The window opens where the ionosphere stops reflecting, and closes where the atmosphere and the available hardware make the link impractical.

The radio spectrum from 1 MHz to 100 GHz with the satellite bands marked A logarithmic frequency axis. Below about 30 MHz waves are reflected by the ionosphere. The satellite bands L, S, C, X, Ku, K and Ka occupy the region from 1 GHz to 40 GHz, and the range from 1 to 12 GHz is marked as the classical satellite window. reflected by the ionosphere 30 MHz practical reflection limit L S C X Ku K Ka 1 to 12 GHz: where satellite systems stayed for decades 1 MHz 10 MHz 100 MHz 1 GHz 10 GHz 100 GHz logarithmic frequency axis
The notes record where the balance settled: limited by the available technologies, satellite systems stayed for decades between \(1\) and \(12\ \text{GHz}\) — the L, S, C and X bands.

06 — Satellite bands

The bands by name, range and use

BandFrequencyWavelengthTypical satellite services
L\(1\)–\(2\ \text{GHz}\)\(30\)–\(15\ \text{cm}\)Mobile satellite services and satellite navigation; small, non-directive terminals.
S\(2\)–\(4\ \text{GHz}\)\(15\)–\(7.5\ \text{cm}\)Mobile services, and telemetry, tracking and command.
C\(4\)–\(8\ \text{GHz}\)\(7.5\)–\(3.75\ \text{cm}\)The classical fixed-satellite service band; robust in rain, but large antennas.
X\(8\)–\(12\ \text{GHz}\)\(3.75\)–\(2.5\ \text{cm}\)Government and military fixed services; radar and imaging.
Ku\(12\)–\(18\ \text{GHz}\)\(2.5\)–\(1.67\ \text{cm}\)Broadcast satellite services and VSAT networks; small dishes, more rain fade.
Ka\(26.6\)–\(40\ \text{GHz}\)\(1.13\)–\(0.75\ \text{cm}\)High-throughput links and very small terminals; strongly rain-affected.

Ranges follow the IEEE column of Table 3 in the Rohde & Schwarz Satellite Technologies guide held in the course reference library, which also places K band between Ku and Ka, from \(18\ \text{GHz}\) up to the start of Ka. Band boundaries differ between the IEEE, ITU and NATO conventions, so always state which convention you are quoting.

06 — Satellite bands

So why not simply go as high as possible?

If every argument pointed upward there would be one band and no discussion. Several bands exist because the arguments disagree:

Moving to a higher frequency
HelpsSmaller antennas for the same beam; more absolute bandwidth available; less congested spectrum; further above the ionospheric limit and its variability.
HurtsStronger interaction with the lower atmosphere, rain in particular; tighter pointing tolerance, because the beam that was easier to form is also easier to miss; harder and more expensive hardware.
ConstrainsWhat technology can actually deliver at acceptable power and cost, and what the international allocations permit for that service.

Frequency selection is a system decision: propagation, antennas, bandwidth, hardware, interference and regulation together. No single band is "the" satellite frequency.

Part 3 — the consequence

We have entered microwave engineering

Choosing gigahertz was a propagation and antenna decision. It is also a hardware decision, and from here the problem changes character: at these frequencies the connection between the source and the antenna stops being a detail.

07 — Microwave engineering

Source → transmission line → antenna → channel

The transmit and receive microwave chains On transmit, a microwave source feeds a transmission line, which feeds an antenna, which radiates into the space channel. On receive, the channel feeds an antenna, a transmission line and then the receiver. The transmission line blocks are highlighted as this week's subject. microwave source transmission line antenna receiver transmission line antenna space channel — uplink space channel — downlink this is the part we have not built yet and the rest of this lecture is about it
Everything outside the gold boxes we have either covered or will meet later. The gold boxes are the question: how do you carry gigahertz power from a source to an antenna without losing it?

08 — Transmission lines

At microwave frequencies, a wire stops being a wire

In a low-frequency circuit a connecting wire is an ideal node: the same voltage appears at both ends at the same instant. That picture quietly assumes the wire is much shorter than a wavelength.

At \(12\ \text{GHz}\) the free-space wavelength is \(25\ \text{mm}\). A \(50\ \text{mm}\) connection is two whole wavelengths long. The consequences are immediate:

Voltage varies along the line

\(V\) and \(I\) are now functions of position as well as time, not single circuit values.

The structure guides a wave

Energy travels as a field between conductors, so the geometry of the structure is part of the circuit.

Loss and radiation matter

Conductor loss rises with frequency, and an open structure radiates the power we were trying to deliver.

So the connection becomes a designed component in its own right: a transmission line.

08 — Transmission lines

Three ways to guide the energy

Cross-sections of a two-wire line, a coaxial line and a hollow waveguide Three transmission-line cross-sections side by side: an open two-wire line, a shielded coaxial line with an inner conductor, and a hollow rectangular waveguide with a single conducting wall. An arrow beneath indicates increasing frequency from left to right. two-wire line coaxial line hollow waveguide two conductors, open field escapes, so it radiates two conductors, shielded field confined by the outer wall one conductor, nothing inside low loss, high power handling typical preference as frequency rises
These ranges overlap heavily; coaxial line is used well into the microwave region and waveguide is used below it. What changes with frequency is which one is the better engineering choice, not where a hard boundary lies.

08 — Transmission lines

What actually drives the choice

Conductor lossRises with frequency and concentrates in a thin surface layer. The notes record that above about \(1\ \text{GHz}\) two-conductor lines become impractical for long runs because of it.
Dielectric lossA coaxial line needs a dielectric to hold the inner conductor in place, and that dielectric absorbs. An air-filled guide has almost none.
Power handlingHollow air-filled waveguides handle much higher power than coaxial cables or printed lines — which matters for a high-power transmit chain.
Dimensions and hardwareWaveguide is bulky and rigid, and its size is set by the operating frequency. Coax and printed lines are small, flexible and cheap to connect.

This is why the notes conclude that waveguides are very important for satellite communications: in the high-power, low-loss parts of a microwave chain, the trade comes out in their favour.

From the original lecture notes · Topic 3, p. 7 →

Part 4 — the structure

Can a wave travel through a hollow metal pipe?

There is no second conductor, no signal wire, no return path. Just air, surrounded by metal. It is worth pausing on how unreasonable this sounds before finding out that it works.

09 — Inside a waveguide

Yes — but not just any field

A wave entering a hollow rectangular metal pipe A sinusoidal wave travels from the left into the open end of a hollow rectangular metal pipe drawn in perspective. A question mark inside the pipe asks whether the wave can continue. ? a wave arrives… …can it continue? conducting walls a tangential electric field cannot exist on them hollow inside no centre conductor, no dielectric — just air so: only certain field patterns fit the allowed patterns are called modes
The answer is yes. But the walls impose conditions the field must satisfy, and only particular field distributions can meet them. Those allowed distributions are the guide's modes.

09 — Inside a waveguide

The geometry, and the pattern it allows

Rectangular waveguide dimensions and the dominant-mode field pattern On the left, a rectangular waveguide in perspective with the broad dimension a, the narrow dimension b and the propagation direction z. On the right, the guide cross-section with vertical electric-field arrows whose length follows a half sine arch across the broad dimension, vanishing at both side walls. a b z conducting (PEC) walls by convention, a is larger than b x = a y = b x y E the field must vanish at both side walls — that is what fixes the pattern
The broad dimension \(a\), the narrow dimension \(b\), and propagation along \(z\). The arrows show the electric field of the simplest allowed pattern: vertical everywhere, strongest in the middle, zero at the two side walls.

From the original lecture notes · Topic 3, p. 10 →

09 — Inside a waveguide

Naming the modes: TEM, TE and TM

Modes are classified by what the field does along the direction of travel, taken here as \(z\):

TEM\(E_z=H_z=0\): both fields entirely transverse. This is the free-space plane wave, and it exists on two-conductor transmission lines — but not inside a hollow waveguide.
TE\(E_z=0\): no electric field along the direction of travel. The dominant mode of a rectangular guide is \(TE_{10}\); of a circular guide, \(TE_{11}\).
TM\(H_z=0\): no magnetic field along the direction of travel. These are higher-order modes and are usually not the ones we operate on.

The two subscripts \(m\) and \(n\) count how the field varies across the cross-section — \(m\) along the broad dimension \(a\), \(n\) along the narrow dimension \(b\). \(TE_{10}\) therefore means one half-cycle of variation across \(a\) and none across \(b\): exactly the arch in the previous figure.

From the original lecture notes · Topic 3, p. 16 →

Part 5 — the rules underneath

Why can a wave propagate at all — in space, and inside a pipe?

Both answers come from the same four equations. We have needed them twice now: once for the wave that crosses the ionosphere, and once for the pattern that fits inside the guide.

10 — Maxwell's equations

The four rules the fields must obey

Equation (1)
\[\nabla\times\mathbf E=-\frac{\partial \mathbf B}{\partial t}\]
Faraday's law

A magnetic field that changes in time creates an electric field.

Equation (2)
\[\nabla\times\mathbf H=\frac{\partial \mathbf D}{\partial t}\]
Ampère–Maxwell law

An electric field that changes in time creates a magnetic field.

Equation (3)
\[\nabla\cdot\mathbf D=\rho_v\]
Gauss's law

Electric charge is the source of the electric field.

Equation (4)
\[\nabla\cdot\mathbf B=0\]
Gauss's law for magnetism

There is no magnetic charge: no isolated north or south pole exists.

Equations (3) and (4) say where fields come from, and neither contains time. Equations (1) and (2) couple the two fields together, and they are the pair that makes propagation possible. \(\mathbf D=\varepsilon\mathbf E\) and \(\mathbf B=\mu\mathbf H\) tie the fields to the medium. Topic 3, p. 8 →

10 — Maxwell's equations

The coupling is what makes a wave

The coupling between a changing electric field and a changing magnetic field A changing electric field creates a magnetic field through equation two, and that changing magnetic field creates an electric field through equation one, so the pair sustains itself and advances. changing E an electric field varying in time changing H a magnetic field varying in time equation (2) — creates equation (1) — creates each cycle of the loop hands the disturbance a little further along z
The displacement current \(\partial\mathbf D/\partial t\) in equation (2) is Maxwell's own contribution, and it is the reason a satellite link is possible at all: a changing electric field makes a magnetic field with no conductor and no charge present.

10 — Maxwell's equations

Four coupled equations become one

  1. Assume a source-free, homogeneous, linear medium: \(\rho_v=0\) so \(\nabla\cdot\mathbf E=0\), with \(\varepsilon\) and \(\mu\) constant. Free space satisfies all of this exactly; so does the air inside a waveguide.
  2. Equations (1) and (2) each contain both fields. Eliminate one by taking the curl of (1): \(\nabla\times(\nabla\times\mathbf E)=-\dfrac{\partial}{\partial t}(\nabla\times\mathbf B)\).
  3. Substitute \(\mathbf B=\mu\mathbf H\) and then (2), \(\nabla\times\mathbf H=\varepsilon\,\partial\mathbf E/\partial t\). The right-hand side becomes \(-\mu\varepsilon\,\partial^{2}\mathbf E/\partial t^{2}\), and \(\mathbf H\) has gone.
  4. On the left use \(\nabla\times(\nabla\times\mathbf E)=\nabla(\nabla\cdot\mathbf E)-\nabla^{2}\mathbf E\); the first term vanishes by step 1, leaving \(-\nabla^{2}\mathbf E\).

Starting from the curl of (2) instead gives the same equation in \(\mathbf H\). The two fields obey the same law, which is another way of saying they are two aspects of one wave.

10 — Maxwell's equations

The result, and the speed it predicts

\[\nabla^{2}\mathbf E=\mu\varepsilon\,\frac{\partial^{2}\mathbf E}{\partial t^{2}}\]

This is the wave equation, the same form a vibrating string obeys: \(\nabla^{2}f=\frac{1}{v^{2}}\partial^{2}f/\partial t^{2}\). Comparing the two fixes the propagation velocity:

\[v=\frac{1}{\sqrt{\mu\varepsilon}},\qquad\quad c=\frac{1}{\sqrt{\mu_0\varepsilon_0}}\approx3\times10^{8}\ \text{m/s}\]

Two constants measured with batteries and magnets predict the speed of light.

From the original lecture notes · Topic 3, p. 9 →

10 — Maxwell's equations

The free-space solution, and its parameters

Working one frequency at a time, every quantity varies as \(e^{j\omega t}\) and the wave equation becomes the form the notes write as equation (5), \(\nabla^{2}\mathbf E+k^{2}\mathbf E=0\) with \(k^{2}=\omega^{2}\mu_0\varepsilon_0\). For a wave travelling along \(z\) with its electric field along \(x\), one solution is equation (6):

\[\mathbf E=\hat a_x\,E_0\,e^{j(\omega t-\beta z)},\qquad \beta=k=\omega\sqrt{\mu_0\varepsilon_0}=\frac{\omega}{c}\]

\(\omega=2\pi f\) is radians of phase per second at a fixed position — the cycle counted in time, fixed by the transmitter.

\(\beta=2\pi/\lambda\) is radians of phase per metre at a fixed instant — the cycle counted in space. The notes call it the phase constant.

A crest keeps \(\omega t-\beta z\) constant, so it advances at \(v=\omega/\beta=f\lambda\). In free space that is \(c\), and \(\lambda=c/f\) — the relation the whole antenna argument rested on.

10 — Maxwell's equations

Every symbol is a feature of the picture

Anatomy of a travelling sinusoidal wave A cosine wave plotted against distance, with the amplitude marked from the axis to the first crest, the wavelength marked between two successive crests, and a second pale copy of the wave shifted to the right to show it travelling. E₀ amplitude λ — one wavelength the whole pattern advances at v = c z solid: the field now  ·  pale: the same field a moment later
Freeze time and the field varies with \(z\) through \(\beta z\); stand at one place and it varies with \(t\) through \(\omega t\). Both \(\lambda\) and \(\beta\) will change once we put this wave inside a metal pipe.

Part 6 — the design rules

Maxwell plus metal walls gives modes and cutoff

The same equations, solved in the same way, but now with a boundary condition: the electric field tangential to a conducting wall must vanish. Everything practical about waveguide design comes out of that one extra requirement.

11 — Modes and cutoff

The same wave equation, with walls

Inside the hollow guide the region is still source free, so the field still satisfies \(\nabla^{2}\mathbf E+k^{2}\mathbf E=0\). What is new is that the solution must also vanish on the conducting walls. The notes give the resulting field as equation (8):

\[\mathbf E=\hat a_y\,E_0\sin\!\left(\frac{\pi x}{a}\right)e^{j(\omega t-\beta z)}\]

The \(\sin(\pi x/a)\) factor is the arch in the figure: it is zero at \(x=0\) and at \(x=a\), which is exactly what the side walls demand. Substituting back gives equations (9) and (10):

\[k^{2}=\left(\frac{\pi}{a}\right)^{2}+\beta^{2}=\omega^{2}\mu_0\varepsilon_0\qquad\Longrightarrow\qquad \beta=\sqrt{\omega^{2}\mu_0\varepsilon_0-\left(\frac{\pi}{a}\right)^{2}}\]

From the original lecture notes · Topic 3, p. 10 →

11 — Modes and cutoff

What that square root is telling us

Dispersion relations for free space and for a waveguide Phase constant beta plotted against angular frequency omega. In free space it is a straight line through the origin of slope one over c. Inside the guide the curve starts at the cutoff frequency and approaches the free-space line from below; below cutoff there is no real beta. β ω ωc below cutoff: the square root is imaginary, so no travelling wave exists free space: β = ω/c inside the guide β is real only above ωc, and always smaller than in free space far above cutoff the guide behaves almost like free space; near cutoff it does not behave like free space at all
In free space \(\beta=\omega/c\) is a straight line, so every frequency propagates. Inside the guide \(\beta\) is real only above a threshold — and that threshold is the cutoff frequency.

11 — Modes and cutoff

Every mode has its own cutoff frequency

Every allowed field pattern has its own cutoff. For an air-filled rectangular guide the notes give equation (14):

\[f_{c,mn}=\frac{c}{2}\sqrt{\left(\frac{m}{a}\right)^{2}+\left(\frac{n}{b}\right)^{2}}\]
\[\text{a mode propagates only if}\quad f>f_{c}\]

Below its cutoff a mode does not travel down the guide at all: the field decays away from the source instead.

Here \(m=0,1,2,\dots\) and \(n=0,1,2,\dots\), not both zero. Topic 3, p. 12 →

11 — Modes and cutoff

Which mode appears first?

The mode with the lowest cutoff frequency is called the dominant mode — it is the first pattern an electromagnetic wave can take inside the guide. Put \(m=1,\ n=0\) into the general formula, with \(a>b\):

\[f_{c,10}=\frac{c}{2a}\]

It depends on the broad dimension \(a\) alone. This is a design equation: choose \(a\), and you have chosen the lowest frequency the guide will carry.

That is the mode whose field we drew earlier: one half-cycle across \(a\), no variation across \(b\), electric field everywhere vertical. Its cutoff wavelength is \(2a\) — the guide must be at least half a wavelength wide before anything can propagate at all.

11 — Modes and cutoff

Check yourself

3 · A quick cutoff

An air-filled rectangular waveguide has \(a=20\ \text{mm}\). Roughly what is its dominant-mode cutoff, and what happens to a \(5\ \text{GHz}\) signal fed into it?

12 — Design: a 12 GHz feed

We need to carry a 12 GHz satellite signal

A ground terminal operates at \(f=12\ \text{GHz}\), a frequency representative of Ku-band satellite downlinks. We have to get that signal from the equipment to the feed of the dish. What waveguide can we use?

\[\lambda_0=\frac{c}{f}=\frac{3\times10^{8}}{12\times10^{9}}=25\ \text{mm}\]

Four questions decide the answer, and we will work through them in order:

1 · Does it propagate?

Is \(f\) above the dominant-mode cutoff of the guide we are considering?

2 · Is it single-mode?

Is \(f\) below the cutoff of the next mode up?

3 · Is there margin?

Is \(f\) comfortably clear of both edges, rather than sitting on one?

12 — Design: a 12 GHz feed

Question 1 — will 12 GHz propagate?

  1. Take a standard rectangular guide with \(a=22.86\ \text{mm}\) and \(b=10.16\ \text{mm}\). Note \(b<a/2\), which is the industry convention the notes describe.
  2. Dominant-mode cutoff: \(f_{c,10}=\dfrac{c}{2a}=\dfrac{3\times10^{8}}{2\times0.02286}=6.56\ \text{GHz}\).
  3. Compare with the operating frequency: \(12\ \text{GHz}>6.56\ \text{GHz}\).
\[f=12\ \text{GHz}\;>\;f_{c,10}=6.56\ \text{GHz}\quad\checkmark\]

The \(TE_{10}\) mode propagates. Question 1 is answered — but on its own, that is not enough to call the design finished.

12 — Design: a 12 GHz feed

Question 2 — what else can propagate?

If the guide is large enough, higher-order modes propagate too. Each one travels at its own rate, so a signal split between modes arrives smeared — what the notes call intermodal distortion. We want exactly one mode in the operating band.

  1. Next mode along the broad wall: \(f_{c,20}=\dfrac{c}{a}=13.12\ \text{GHz}\).
  2. First mode across the narrow wall: \(f_{c,01}=\dfrac{c}{2b}=14.76\ \text{GHz}\).
  3. So at \(12\ \text{GHz}\) only \(TE_{10}\) propagates — but the next mode begins just \(1.1\ \text{GHz}\) higher.
  4. The notes give the recommended band as \(1.2f_{c,10}<f_{op}<0.8f_{c,20}\), which here is \(7.87\)–\(10.50\ \text{GHz}\).

12 — Design: a 12 GHz feed

Question 3 — so choose a smaller guide

Shrinking \(a\) raises every cutoff frequency together, sliding the whole single-mode window upward until it contains \(12\ \text{GHz}\):

a = 22.86 mma = 19.05 mm
\(f_{c,10}=c/2a\)6.56 GHz7.87 GHz
\(f_{c,20}=c/a\)13.12 GHz15.75 GHz
Recommended band7.87 – 10.50 GHz9.45 – 12.60 GHz
Is 12 GHz inside?No — above the windowYes

The second guide, with \(a=19.05\ \text{mm}\) and \(b=9.525\ \text{mm}\), carries \(12\ \text{GHz}\) in a single mode with margin at both edges. That is the answer to the design question.

From the original lecture notes · Topic 3, p. 13 →

12 — Design: a 12 GHz feed

The wave is longer inside the guide

Rewriting the notes' \(\beta=\sqrt{\omega^{2}\mu_0\varepsilon_0-(\pi/a)^{2}}\) in terms of the cutoff frequency gives the two quantities a microwave engineer works with:

\[\beta=k_0\sqrt{1-\left(\frac{f_c}{f}\right)^{2}},\qquad \lambda_g=\frac{2\pi}{\beta}=\frac{\lambda_0}{\sqrt{1-\left(f_c/f\right)^{2}}}\]

The square root is always less than one, so \(\lambda_g>\lambda_0\): the wavelength along the guide is always longer than in free space, and it stretches without limit as \(f\) approaches cutoff. For our chosen guide at \(12\ \text{GHz}\), \(\lambda_g=33.1\ \text{mm}\) against \(\lambda_0=25\ \text{mm}\), and \(\beta=2\pi/\lambda_g=190\ \text{rad/m}\).

\(\beta\) is the phase change per metre along the guide — the quantity that sets the electrical length of every section of the feed, and the reason a waveguide run cannot be measured in free-space wavelengths.

12 — Design: a 12 GHz feed

Check yourself

4 · Two things to avoid

Why should a waveguide feed be operated neither too close to cutoff nor in an arbitrarily large guide?

13 — Putting it back together

From a spacecraft in orbit to a waveguide dimension

Every step in this lecture was forced by the one before it. Read the chain backwards and the waveguide on the bench is explained by an orbit.

  1. pick a frequency
  2. cross the ionosphere
  3. get directivity
  4. so: microwaves
  5. feed the antenna
  6. so: waveguide
  7. modes & cutoff
The ionospheresets a floor: reflection below roughly \(30\ \text{MHz}\), so an Earth–space link must sit far above it.
Directivityraises the floor much further: \(D\propto A/\lambda^{2}\), so a buildable antenna needs a small \(\lambda\), which means GHz.
Microwave hardwarethen makes the feed a design problem, and low loss with high power favours waveguide.
Maxwell plus wallsgives modes, a cutoff for each, and \(f_{c,10}=c/2a\) — which turns the operating frequency into a dimension in millimetres.

13 — Putting it back together

Carry these forward

Frequency floor

\(f_{\text{critical}}=9\sqrt{N_{\max}}\); with obliquity the practical reflection limit is about \(30\ \text{MHz}\).

Why microwaves

\(\lambda=c/f\) and \(D\propto A/\lambda^{2}\): a fixed dish is electrically larger, and far more directive, at higher \(f\).

Why waveguide

Above about \(1\ \text{GHz}\), low loss and high power handling favour a hollow single-conductor guide.

Cutoff

\(f_{c,mn}=\frac{c}{2}\sqrt{(m/a)^{2}+(n/b)^{2}}\), dominant \(f_{c,10}=c/2a\), and a mode travels only if \(f>f_c\).

EE 499 · Week 5

Week 5 complete

  1. frequency
  2. ionosphere
  3. directivity
  4. microwaves
  5. transmission lines
  6. waveguide modes

We started with a spacecraft in a known orbit and finished holding a waveguide whose width is set by the frequency we chose in the first ten minutes. Nothing in that chain was arbitrary: the ionosphere set a floor, directivity pushed us to microwaves, and microwaves made the feed a design problem with its own equations.

Next: Week 6 turns the waveguide dimension into hardware — circular guides, standard sizes including WR-340, and coaxial cable. Week 7 then looks inside the guide at the field itself, and Week 8 asks what happens at the joints, loads and components along the path.

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