MASINDE MULIRO UNIVERSITY OF SCIENCE AND TECHNOLOGY
Department of Electrical & Communication Engineering

INTRODUCTION TO SPACE WAVE COMMUNICATION

Line-of-Sight Propagation of VHF, UHF and Microwave Signals
Course: ECE 523E — Antennas & Radiowave Communication
Level: 5th Year, Electrical & Communication Engineering
Topic: Introduction to Space Wave Communication — LOS Geometry, Path Loss, Multipath & Link Design

Learning Objectives

By the end of this lecture the student should be able to:

  1. Define the space wave, identify the frequency bands in which it is the dominant mode, and distinguish it from the ground and sky waves.
  2. Compute the radio horizon, earth bulge and required antenna heights for a given line-of-sight path.
  3. Apply the Friis transmission formula and free-space path-loss equation to point-to-point links.
  4. Analyse the two-ray (plane-earth) model: path difference, phase reversal, break distance and the 1/d⁴ far-field law.
  5. Assess obstruction effects using knife-edge diffraction and the Fresnel-zone clearance criterion.
  6. Explain tropospheric refraction, the k-factor and ducting.
  7. Characterise multipath fading and select appropriate countermeasures (diversity, equalisation).
  8. Use standard empirical path-loss models (Okumura–Hata) in coverage studies.
Figure 1
Fig. 1 — The space wave travels essentially in a straight line from transmitting to receiving antenna — path geometry is everything.

Propagation Modes — Where the Space Wave Fits

Figure 2
Fig. 2 — The three basic propagation modes; the space wave (b) dominates at VHF and above.
ModeBandRange
Ground waveVLF, LF, MF≤ a few hundred km (surface-guided)
Sky waveHF (3–30 MHz)Intercontinental via ionosphere
Space waveVHF 30–300 MHz, UHF 300 MHz–3 GHz, SHF > 3 GHzLine of sight (≈ radio horizon)
Why VHF and above? The ionosphere is transparent to frequencies above ~30 MHz (they penetrate it instead of being refracted back), and ground-wave loss becomes prohibitive — so the wave simply travels straight through the troposphere.
Consequence: coverage of a space-wave link is set by antenna heights and path geometry, not by ionospheric conditions — but it is subject to terrain, buildings, and multipath interference.

What is the Space Wave?

Definition

The space wave is the component of the radiated field that reaches the receiver along a (practically) straight path through the lower atmosphere — either directly, or after reflection from the ground or scattering from objects along the route.

Composition

  • Direct (LOS) component — the straight TX→RX path.
  • Ground-reflected component — reflected once (or more) from the earth's surface.
  • Scattered/diffracted components — from terrain, buildings and vegetation (dominant in mobile urban channels).

Typical applications

FM/TV broadcasting, cellular and Wi-Fi networks, point-to-point microwave backhaul, radar, satellite up/down-links (the wave traverses the ionosphere as a space wave).

The space wave is the working horse of modern wireless: nearly all systems above 100 MHz are space-wave systems.

Key properties

  • Propagates in the troposphere (0–10 km) — weather-dependent refraction matters.
  • Obey free-space spreading (1/d² in power) only when no ground reflection interferes.
  • Links are engineered for a specified path clearance (Fresnel criterion) rather than mere visual LOS.
  • Multipath is the defining impairment: constructive/destructive interference of the components above.

Quick numbers

Radio horizon: d (km) = 4.12√(h in m)
Examples: h = 10 m → 13 km; h = 30 m → 22.6 km; h = 100 m → 41 km; h = 300 m → 71 km
Earth bulge at mid-path: h$_b$ (m) = d$_1$·d$_2$ / 12.75   (d in km)

Line-of-Sight Geometry & the Radio Horizon

Figure 3
Fig. 3 — LOS geometry over a spherical earth: the radio horizon exceeds the optical horizon because atmospheric refraction bends rays toward the earth (effective earth radius kR, standard k = 4/3).

Radio horizon vs optical horizon

  • Optical horizon: d = 3.57√h — light rays are not refracted appreciably.
  • Radio horizon: d = 4.12√h — the standard atmosphere bends radio rays downward, extending the horizon by ~15%.
  • Maximum LOS distance between two antennas: d$_{max}$ = 4.12(√h$_1$ + √h$_2$) km.

Worked micro-example

Two 30 m towers: d$_{max}$ = 4.12(√30 + √30) = 4.12 × 2 × 5.48 ≈ 45 km. A 25 km link is comfortably within LOS, but path clearance (Fresnel criterion, slide 12) still must be verified.

Engineering rule: never design exactly "to the horizon" — atmospheric variability (k-factor swings, ducting) means fading margin and clearance criteria are always added on top of the nominal geometry.

Free-Space Path Loss & the Friis Equation

Figure 4
Fig. 4 — Free-space path loss vs distance at several frequencies: 20 dB/decade with distance and 20 dB/decade with frequency.

Friis transmission equation

P$_r$ = P$_t$ G$_t$ G$_r$ ( λ / 4πd )²

Free-space path loss

L$_{FS}$ (dB) = 20log(4πd/λ) = 32.44 + 20log f(MHz) + 20log d(km)

Reading the chart

  • Going from 1 km to 10 km costs 20 dB; from 1 GHz to 10 GHz costs another 20 dB.
  • Higher frequencies give more antenna gain for a fixed aperture — the extra FSPL is often recovered at the antennas (G ∝ f² for a fixed-dish antenna), which is why microwave links favour high bands.
  • "Free-space loss" is not absorption — it is simply the spreading of power over the spherical wavefront (inverse-square law).
Friis applies strictly only in free space — real space-wave links obey it up to the break distance, after which ground reflection takes over (next slides).

Ground Reflection — the Two-Ray Model

Why reflection matters

For terrestrial LOS links the antennas are close to the ground, so the wave reflected from the earth's surface arrives at the receiver with a delay of only a few nanoseconds and a phase reversal (R ≈ −1 at grazing angles). Direct and reflected rays then interfere.

Key relations

Path difference: Δ ≈ 2h$_1$h$_2$/d
Total phase difference: Δφ = (2π/λ)·Δ + π

At grazing angles Δφ ≈ π and the two rays cancel almost perfectly — the receiver field is set by the difference of the two nearly-equal phasors, which grows with Δ (i.e. with h₁h₂ and with 1/d):

E ≈ 2E$_0$ sin(2πh$_1$h$_2$ / λd)  ≈  E$_0$·(4πh$_1$h$_2$ / λd)   (small argument)
The received power therefore falls as 1/d⁴ (field ∝ 1/d²) beyond a break distance — 12 dB per decade worse than free space.
Figure 5
Fig. 5 — Two-ray geometry: the direct ray and the ground-reflected ray (image construction). Reflection near grazing incidence introduces a π phase reversal.

Two-Ray Path Loss & the Break Distance

Figure 6
Fig. 6 — Path loss vs distance for h₁ = h₂ = 30 m at 900 MHz: free-space 1/d² up to the break distance d_b ≈ 10.8 km, then 1/d⁴.

The break distance

d$_b$ = 4h$_1$h$_2$ / λ
  • For d ≪ d$_b$: path difference Δ ≪ λ — the rays cancel almost completely; received power follows free space (1/d²) modulated by interference nulls.
  • For d ≫ d$_b$: the phase difference grows with distance and |sin(·)| → its envelope; power falls as (h₁h₂)²/d⁴.

Design formulas

P$_r$ (d ≫ d$_b$) = P$_t$ G$_t$ G$_r$ (h$_1$²h$_2$² / d⁴)   [linear]
P$_r$ (dB) = P$_t$ + G$_t$ + G$_r$ + 40log(h$_1$h$_2$ / d²) + constant
Raising either antenna height extends coverage dramatically (∝ h² in power). This is why cellular towers and microwave masts are tall — and why mobile-phone coverage is height-dominated.

Effect of Antenna Heights and Frequency

Reading the chart

  • Doubling antenna height moves the break distance 4× farther and lowers the whole 1/d⁴ branch by 12 dB.
  • At a fixed distance, higher frequency moves d$_b$ out too (∝ f) — but the absolute path loss still grows with f² in the near region.
  • In the interference region (d < d$_b$) the curves show the classic two-ray nulls — deep fades at distances where Δφ = odd multiples of π. The last null before d$_b$ occurs near 0.7·d$_b$.
The two-ray model explains a classic mobile-network observation: a handset at ground level in a flat rural area loses signal faster (≈ 40 dB/decade) than one in an urban area where scattering breaks up the clean interference pattern (≈ 30–35 dB/decade, Hata urban).
Figure 7
Fig. 7 — Break distance moves outward with antenna height and with frequency (d_b = 4h₁h₂/λ). The markers show the break point of each curve.

Diffraction — Obstructions on the Path

Figure 8
Fig. 8 — (a) Knife-edge diffraction geometry and the Fresnel parameter v. (b) Diffraction loss vs v — even a grazing obstruction costs ~6 dB, and loss grows steeply beyond.

Knife-edge diffraction

  • When the LOS path is blocked by a ridge, roof edge or building corner, the wave still bends around it — diffraction.
  • The obstruction is characterised by the dimensionless Fresnel parameter v; losses of 6–20 dB are typical for marginal obstructions.
v = h·√[ 2(d$_1$+d$_2$) / (λ d$_1$ d$_2$) ]
  • v < 0: LOS clear (loss ≈ 0, small ripple).
  • v = 0: grazing — ≈ 6 dB.
  • v > 0: obstruction above LOS — loss rises ~monotonically with v.
Fresnel zones (next slide) give the practical clearance rule: the first Fresnel zone must be kept at least 60% unobstructed to keep diffraction loss small.

Fresnel Zones & the Clearance Criterion

Fresnel zones

The n-th Fresnel zone is the locus of points where the path length TX→P→RX exceeds the LOS path by nλ/2. The first zone carries most of the energy — it must be protected.

F$_n$(s) = √[ n·λ·s(d−s) / d ]

The 0.6 F₁ rule

  • Keep the path clear of obstructions to at least 60% of the first-zone radius everywhere along the path.
  • Better clearance (≥ 1.0 F₁) is specified for high-availability links; obstacles within the first zone cause partial cancellation (diffraction loss) even though the path is "visually clear".
Worked micro-example: 2 GHz (λ = 0.15 m), d = 20 km. F₁ at mid-path = ½√(λd) ≈ 27 m → keep obstacles below ≈ 16 m along the route. This is why 20 km microwave hops need ~20–30 m towers even with clean LOS.
Figure 9
Fig. 9 — (a) Fresnel ellipses (r₁+r₂ = d + nλ/2) — an obstruction piercing the first zone adds diffraction loss. (b) First-zone radius vs path position; the 60% clearance line is the design limit.

Tropospheric Refraction, k-Factor & Ducting

Figure 10
Fig. 10 — Effect of atmospheric refractive-index gradient on a space-wave ray: standard (k = 4/3), super-refraction, and ducting in an anomalous layer.

Effective earth radius

Because refractive index n decreases with height, rays bend toward the denser (lower) air. The effect is modelled by scaling the earth radius by the k-factor:

R$_e$ = k·R,   standard atmosphere: k = 4/3

Variability

  • Sub-refraction (k < 4/3, e.g. cool moist air): rays bend less → LOS paths can unexpectedly lose clearance ("earth bulge grows").
  • Super-refraction (k > 4/3): extended ranges — coastal/sea-breeze conditions.
  • Ducting (k < 0): rays trapped in a layer → anomalous interference over hundreds of km; a major problem for frequency-reuse microwave networks.
Design responses: over-water paths checked with k = 4/3 nominal down to k ≈ 2/3 worst-case; hop lengths and antenna heights chosen against multipath outage objectives (ITU-R P.530).

Atmospheric Absorption & Rain Attenuation (SHF/EHF)

Figure 11
Fig. 11 — (a) Gaseous absorption vs frequency: the 60 GHz oxygen band and water-vapour lines at 22 and 183 GHz define the low-loss "windows" used by microwave and mmWave links. (b) Rain specific attenuation grows rapidly with frequency and rain rate.

Gaseous absorption

  • Resonant absorption by O₂ (~60 GHz) and H₂O vapour (22, 183 GHz) adds γ·d dB to the link loss.
  • Below ~10 GHz, gaseous loss (< 0.01 dB/km) is negligible — ignored in the Friis budget.
  • The 60 GHz oxygen band (~15 dB/km) both limits and enables systems: short-range 5G/WiGig links reuse spectrum freely since signals cannot travel far.

Rain attenuation

  • Above ~10 GHz, rain becomes the dominant weather impairment: γR = k·Rα dB/km, with k, α from ITU-R P.838 and R the rain rate (mm/h).
  • Design is availability-based: e.g. a 30 GHz, 5 km hop in heavy rain (50 mm/h) loses ~0.5–1 dB/km → 3–5 dB — covered by a rain-fade margin; deeper fades (0.01% of time) need site diversity or adaptive coding.
Total path loss: L = L$_{FS}$ + γ$_{gas}$·d + γ$_{R}$·d + L$_{cloud/fog}$
Rule of thumb for link planning: below 10 GHz design against multipath; 10–30 GHz add rain margin from local statistics; above 30 GHz rain + absorption dominate the budget.

Multipath Fading in Space-Wave Links

Figure 11
Fig. 12 — (a) Fast fading at a moving receiver: multipath echoes sum with time-varying phases, giving rapid 20–30 dB power swings. (b) The same channel is frequency-selective: deep notches move across the band.

Types of fading

TypeCauseCharacter
Flat (narrowband) fadingAll frequency components fade togetherDeep nulls; mitigated by power margin, diversity
Frequency-selective fadingDelay spread ≳ symbol periodISI + notches; mitigated by equalisation, OFDM, RAKE
Slow (shadow) fadingBuildings, terrain blockingLog-normal, σ ≈ 6–10 dB; mitigated by margin, cell planning

Channel parameters

Delay spread τ$_{rms}$ vs symbol time T$_s$: τ$_{rms}$/T$_s$ ≪ 1 → flat;  coherence B$_c$ ≈ 1/(2πτ$_{rms}$)
Small-scale fading statistics are typically Rayleigh (no dominant LOS) or Rician (strong LOS + scattered echoes) — these drive link-margin calculations (e.g. 20 dB margin for ~99% reliability at Rayleigh).

Countermeasures — Diversity & Combining

Diversity principle

Provide the receiver with several statistically independent copies of the signal; the probability that all fade deeply at once is small. Independence is achieved by separating the copies in space, frequency, time, polarisation or angle.

Common techniques

  • Space diversity: two antennas ≥ λ/2 apart (base stations use several wavelengths vertically/horizontally).
  • Frequency diversity: transmit on two separated carriers (traditional microwave; now less used — spectrum cost).
  • Time diversity: interleaving + coding + retransmission (ARQ) — the basis of modern cellular.
  • Polarisation diversity: ±45° slant polarisations at the handset.

Combining

Selection combining (pick strongest) · Equal-gain combining · Maximal-ratio combining (MRC) — optimum, gain ≈ SNR sum
Modern form: MIMO — multiple antennas at both ends exploit multipath as parallel spatial channels instead of fighting it.
Figure 12
Fig. 13 — (a) Space diversity: a second antenna sees an independent fade. (b) Envelope correlation vs spacing in wavelengths: ρ = J₀²(2πs/λ) — spacing of ~λ/2 decorrelates the fades.

Empirical Path-Loss Models — Okumura–Hata

Figure 13
Fig. 14 — Okumura–Hata median path loss at 900 MHz compared with free space: environment (urban → rural) changes the slope and intercept by tens of dB.

Why empirical models?

Two-ray theory assumes a flat, perfectly reflecting earth. Real terrain, clutter and buildings are handled with measurement-based models.

Okumura–Hata (UHF, 150–1500 MHz)

L$_{urban}$ = 69.55 + 26.16log f − 13.82log h$_b$ − a(h$_m$) + (44.9 − 6.55log h$_b$)log d
L$_{suburban}$ = L$_{urban}$ − 2[log(f/28)]² − 5.4
L$_{rural}$ = L$_{urban}$ − 4.78(log f)² + 18.33log f − 40.94

f in MHz, d in km, h$_b$ = base-station height, h$_m$ = mobile height; a(h$_m$) is the mobile antenna correction.

Successors: COST-231 Hata (up to 2 GHz), COST-231 Walfisch–Ikegami (urban microcells), and 3GPP/5G statistical models. Modern tools use ray-tracing calibrated against measurements.

Worked Example — Point-to-Point Microwave Link Budget

Problem. A 2 GHz, 25 km hop between two 25 m towers over average terrain carries an E1 (2 Mbit/s) stream. TX power 30 dBm (1 W), antenna gains 24 dBi each, feeder+connector losses 2 dB each end, receiver sensitivity −85 dBm. Verify the link and the path clearance.

Step 1 — free-space path loss

L$_{FS}$ = 32.44 + 20log(2000) + 20log(25) = 32.44 + 66.02 + 27.96 ≈ 126.4 dB

Step 2 — received power

P$_r$ = 30 + 24 + 24 − 2 − 2 − 126.4 = −52.4 dBm

Step 3 — margin

M = −52.4 − (−85) = 32.6 dB — comfortable even after a 15 dB multipath/degradation allowance

Step 4 — path clearance (Fresnel)

λ = 0.15 m;   F₁(mid) = √[λ·d₁d₂/d] = √[0.15×12500×12500/25000] ≈ 27.4 m
Required: 0.6×27.4 ≈ 16.4 m

Earth bulge at mid-path: h$_b$ = d₁d₂/12.75 ≈ 12.3 m. Clearance from a 25 m tower: 25 − 12.3 ≈ 12.7 m — slightly short of the 16.4 m rule → specify 30 m towers (clearance 17.7 m ✓).

Step 5 — radio horizon check

d$_{max}$ = 4.12(√30 + √30) ≈ 45 km > 25 km ✓
Class exercise: Repeat the budget at 5.8 GHz with 20 dBi antennas. (Answer: L$_{FS}$ ≈ 135.7 dB, P$_r$ ≈ −55.7 dBm — the higher FSPL is largely offset by the larger antenna apertures.)

Applications of Space Wave Communication

SystemBandSpace-wave role
FM sound / TV broadcasting88–108 MHz / 470–860 MHzPrimary coverage mode; range set by transmitter height (radio horizon)
Cellular (2G–5G)700 MHz – 6 GHz (FR1), mmWave FR2Two-ray + multipath channel; Hata/3GPP models; diversity & MIMO
Wi-Fi / WLAN / Bluetooth2.4 / 5 / 6 GHzIndoor multipath; link budgets of tens of dB over rooms/floors
Point-to-point microwave6–42 GHzBackhaul; Fresnel clearance + ITU-R P.530 fading design
Satellite linksUHF–Ka bandWave passes through the ionosphere as a space wave
Radar & GNSS1–40 GHzMonostatic/bistatic space-wave propagation
IoT / LPWAN (LoRa, NB-IoT)sub-GHz / licensed bandsLong-range, low-rate links using the tropospheric space wave

Why engineers still study it

  • Every cellular, Wi-Fi, broadcast and satellite budget in industry starts with the Friis/two-ray framework taught here.
  • Path-loss modelling, fading margin and diversity are the core skills of RF/wireless engineering.
  • 5G/6G techniques (beamforming, massive MIMO, mmWave blockage analysis) extend exactly this LOS + multipath picture.
Career link: this material feeds directly into RF planning tools (Atoll, Planet), drive-test interpretation, and ITU-R-based link planning used by operators and regulators.

Summary & Key Takeaways

  1. The space wave is the dominant mode at VHF and above; it propagates essentially in a straight line through the troposphere.
  2. Coverage is set by antenna height: radio horizon d = 4.12√h (k = 4/3 earth).
  3. Free-space behaviour: Friis formula; L$_{FS}$ = 32.44 + 20log f + 20log d (dB) — 20 dB/decade in distance and frequency.
  4. Ground reflection creates the two-ray channel: break distance d$_b$ = 4h₁h₂/λ; beyond it, power ∝ 1/d⁴.
  5. Keep the first Fresnel zone ≥ 60% clear: F₁ = √[λs(d−s)/d]; obstacles cost knife-edge diffraction loss (≈ 6 dB at grazing).
  6. Refraction bends rays toward the earth (k-factor); ducting gives anomalous interference; plan worst-case clearances.
  7. Multipath → flat/frequency-selective Rayleigh–Rician fading; counter with margin, diversity (ρ = J₀²(2πs/λ)), coding, MIMO.
  8. Real networks use empirical models (Okumura–Hata, COST-231, ray-tracing) for coverage and capacity planning.

Exam-style questions to revise

  • Two 40 m towers at 2.4 GHz: find the break distance and state the far-field path-loss slope. (d$_b$ = 4·1600/0.125 ≈ 51 km.)
  • A 900 MHz base station at 30 m serves 1.5 m handsets 2 km away. For P$_t$ = 40 dBm, G$_t$ = 12 dBi, G$_r$ = 0 dBi, compare the two-ray prediction with free space. (d$_b$ ≈ 540 m → far region; two-ray ≈ free space + 40log(d/d$_b$) ≈ 22 dB worse.)
  • Explain why microwave links need tall towers even when the path is "visually clear".
  • Define delay spread and coherence bandwidth, and state when a 20 MHz LTE channel is flat vs frequency-selective.
  • Why is diversity spacing at the mobile often λ/4 while the base station uses several λ?
Next lecture: Mobile radio channel characterisation — measurement, tapped-delay-line models and simulation in MATLAB.

References & Further Reading

  • Balanis, C. A., Antenna Theory: Analysis and Design, 4th ed., Wiley, 2016 — Ch. 2, 4 (multipath, two-ray, ground effects).
  • Rappaport, T. S., Wireless Communications: Principles and Practice, 2nd ed., Prentice-Hall, 2002 — Ch. 3–4 (path loss, fading, diversity, Hata).
  • Saunders, S. R. & Aragón-Zavala, A., Antennas and Propagation for Wireless Communication Systems, 2nd ed., Wiley, 2007.
  • Goldsmith, A., Wireless Communications, Cambridge University Press, 2005 — fading channels & diversity.
  • Okumura, Y. et al., "Field strength and its variability in VHF and UHF land-mobile radio service," Rev. Elec. Commun. Lab., 1968; Hata, M., "Empirical formula for propagation loss," IEEE Trans. Veh. Technol., 1980.
  • ITU-R P.525 — Calculation of free-space attenuation; P.526 — Diffraction; P.530 — Point-to-point propagation data and prediction methods; P.1546 — Broadcasting coverage prediction.
  • Parsons, J. D., The Mobile Radio Propagation Channel, 2nd ed., Wiley, 2000.
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