Masinde Muliro University of Science and Technology

Space-Wave Communication

ECE 523E — Antenna & Radio Wave Propagation
Comprehensive Study Guide  |  5th Year BSc. Electrical & Communication Engineering

1. Learning Objectives

By the end of this study guide, the student should be able to:

  1. Define the space wave (direct wave) and its component paths, and explain its dominance at VHF and above.
  2. Compute radio-horizon distances using the k = 4/3 effective-earth model, and determine required Fresnel-zone clearances for any link.
  3. Analyse multipath propagation: two-ray interference, the critical distance, the 1/d⁴ law, Rayleigh and log-normal fading statistics.
  4. Quantify diffraction loss over knife edges and smooth spherical earth, and account for atmospheric effects: refraction, ducting, tropospheric scatter and rain attenuation.
  5. Select and apply appropriate path-loss models (free space, two-ray, Okumura–Hata, COST-231, ITU-R P.1546/P.1812) for a given scenario.
  6. Perform space-wave link budgets including antenna gains (dish formula), thermal noise, required C/N, and fading/rain margins.
  7. Specify antennas for point-to-point microwave and satellite links, and solve related numerical problems.

2. Introduction

The space wave is the component of a radio wave that travels the direct (line-of-sight) path through the troposphere between transmitting and receiving antennas — aided and abetted by whatever the local environment provides: ground and building reflections, diffraction around obstacles, and occasional atmospheric ducts.

BandFrequencyRepresentative servicesKey space-wave issue
VHF30–300 MHzFM radio, TV, airband, 2 m amateurHorizon + diffraction; modest rain effect
UHF0.3–3 GHzTV, cellular, GPS, WiFiMultipath, clutter; rain still minor
SHF (microwave)3–30 GHzSatellite C/Ku/Ka, backhaul, radar, 5GRain fade; precise pointing; Fresnel discipline
EHF (mm-wave)30–300 GHz5G mm-wave, automotive radarLOS only; oxygen/rain absorption; tiny beams

Why this is core ECE 523 material: every concept of antenna and propagation engineering converges here — aperture and gain, free-space loss, reflection and diffraction, atmospheric refraction, noise and link budgets. Master the space wave and you can budget any terrestrial or satellite link.

3. Line-of-Sight Geometry and Fresnel Zones

3.1 Radio Horizon

Standard atmospheric refraction bends rays downward, equivalent to an Earth of radius k × R with k = 4/3:

Radio horizon d(km) ≈ 4.12 ( √h1 + √h2 ) , h in metres

Height is coverage: doubling a mast's height adds ≈ 41 % to the horizon radius (d ∝ √h).

3.2 Fresnel Zones — the Volume of LOS

"Line of sight" is not a line but an ellipsoid: secondary waves arriving within the first Fresnel zone add in phase with the direct ray. The engineering rule: keep at least 60 % of the first zone clear.

First-zone radius at a point r₁ = √( λ d₁ d₂ / (d₁ + d₂) )
Maximum (mid-path) r₁max = ½ √( λ d )   (d = total path)

4. Multipath and Reflection

4.1 Two-Ray Model

Over a flat reflecting surface, the received signal is the sum of the direct ray and the ground-reflected ray (reflection coefficient ≈ −1 at grazing incidence). The result is interference with a striking distance law:

Two-ray received power Pr ≈ Pt Gt Gr (h₁² h₂²) / d⁴   (d beyond the critical distance dc ≈ 4h₁h₂/λ)
Interpretation −6 dB/octave in free space becomes −12 dB/octave beyond dc

4.2 Multipath Fading Statistics

Diversity rule of thumb: decorrelate branches by ≥ 10λ (space) or ≥ coherence bandwidth (frequency) so fades do not coincide.

5. Diffraction Loss

When the path is blocked by a ridge, rooftop or building edge, the knife-edge model gives:

Fresnel parameter v = h √( 2(d₁ + d₂) / (λ d₁ d₂) )   (h = obstruction height relative to the LOS line, + into the path)
Knife-edge loss L(v) ≈ 6.9 + 20 log( √( (v − 0.1)² + 1 ) + v − 0.1 ) dB
Reference points v = 0 (grazing): ≈ 6 dB  |  v = 1: ≈ 16 dB  |  v = 2: ≈ 22 dB

6. Atmospheric Effects: Refraction, Ducting, Scatter, Rain

7. Path-Loss Models

ModelApplicabilityFormNotes
Free spaceLOS, clear pathL = 32.44 + 20log f + 20log dThe anchor; never enough outdoors alone
Two-rayLow antennas, open flat groundPr ∝ 1/d⁴ beyond dcExplains mobile slope of ~40 dB/decade
OkumuraUrban UHF (measured curves)Curves + correctionsHistorical basis of cellular planning
Hata / COST-231150–1500 / up to 2 GHzClosed-form urban/suburban/ruralFast, widely used in tools
ITU-R P.1546 / P.1812Point-to-area broadcastField-strength curves + terrainRegulatory standard for coverage

Model selection discipline: match the model to the scenario (height, clutter, frequency), calibrate with measured data, and document the model used in every budget.

8. The Space-Wave Link Budget

Received power Pr(dBm) = Pt + Gt + Gr − Lpath − Lmargin − Lfeeder/misc
Noise N = −174 + 10log B + NF (dBm)
Required C/N ≈ 10 dB (QPSK) · 18 dB (64-QAM) · 24 dB (256-QAM) + implementation loss ~1–3 dB
Fade margin Rayleigh 99.9 % availability ⇒ ~20–30 dB above median; rain per ITU-R P.618 availability targets

9. Antennas for Space-Wave Links

AntennaTypical gainPatternApplications
Dipole / collinear arrays0–8 dBiOmnidirectional azimuthBroadcast, base-station sectors
Yagi–Uda7–15 dBi20–60° beamTV/FM reception, point-to-point
Panel / sector antennas10–20 dBi60–120° azimuthCellular/WiFi access
Parabolic dish25–50 dBi1–10° beamSatellite, microwave backhaul
Horn / grid / Cassegrain10–40 dBiVariousMicrowave, test ranges, feeds
Dish gain G = η (πD/λ)² , η ≈ 0.5–0.7   |   Half-power beamwidth ≈ 70° λ/D

11. Worked Examples

Example 1 — Radio horizon

Find the radio horizon for a 60 m tower and a 3 m rooftop.

Example 2 — Fresnel clearance

A 6 GHz, 30 km microwave hop: find the first-Fresnel-zone maximum radius and the required clearance.

Example 3 — Knife-edge loss

A hill 10 m above the LOS line sits mid-path on a 10 km, 1 GHz link. Estimate the loss.

Example 4 — FSPL and received power

FSPL and Pr for 14 GHz, 15 km, 10 W (+40 dBm), 35 dBi dishes each end, 2 dB feeder loss.

Example 5 — Dish sizing

What diameter dish gives 35 dBi at 12 GHz (η = 0.6)? What is its beamwidth?

Example 6 — Rain margin check

The Example 4 link must survive 99.99 % availability in a region where 0.01 % of the year has rain of 10 mm/h at 14 GHz (γR ≈ 2 dB/km). Check the margin.

Example 7 — Two-ray slope check

A base station (30 m) serves a handset (1.5 m) at 900 MHz. Find the critical distance and the slope beyond it.

12. Interactive Calculators

12.1 Radio Horizon (k = 4/3)


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12.2 Fresnel-Zone Calculator


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12.3 Knife-Edge Diffraction Loss


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12.4 Link Budget Calculator




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12.5 Dish Gain & Beamwidth


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13. Summary of Key Points

  1. The space wave dominates VHF and above: direct path + reflections + diffraction; the channel is geometry, statistics and weather.
  2. Radio horizon d ≈ 4.12(√h₁ + √h₂) km with the k = 4/3 effective earth; height is coverage.
  3. LOS is a volume: r₁ = √(λd₁d₂/(d₁+d₂)), and 60 % of the first Fresnel zone must stay clear.
  4. Two-ray interference gives the 1/d⁴ law beyond the critical distance; multipath yields Rayleigh (small-scale) and log-normal (shadowing) fading — fight with diversity, equalization, OFDM and margin.
  5. Knife-edge loss follows the Fresnel parameter v (0 dB at clearance, 6 dB grazing, 16 dB at v = 1); spherical-earth diffraction gives gradual beyond-horizon fade.
  6. The atmosphere refracts (k factor), ducts (extended interference), scatters (troposcatter links) and rains (γR = kRα above ~10 GHz).
  7. Choose models to match the scenario: FSPL anchor, two-ray mobile, Hata/COST-231 urban, P.1546/P.1812 regulatory.
  8. Link budgets: Pr = Pt + Gt + Gr − losses; N = −174 + 10log B + NF; margins for Rayleigh (20–30 dB) and rain (per availability target).
  9. Antennas: gain ∝ (D/λ)² for dishes, beamwidth ≈ 70°λ/D; pointing and feeder losses matter at microwave.
  10. Microwave backhaul and satellite links are the same discipline at longer distances — complete the whole budget chain before judging feasibility.

14. Self-Test Quiz (12 Questions)

Attempt each question, then click "Check Answers".

1. The space wave is dominant at:

2. The radio horizon formula d(km) ≈ 4.12(√h₁ + √h₂) uses:

3. The required clearance on a line-of-sight path is:

4. Beyond the critical distance in a two-ray channel, received power falls as:

5. Knife-edge diffraction loss at grazing incidence (v = 0) is approximately:

6. Rain attenuation becomes a first-order design term roughly above:

7. A 60 cm dish at 12 GHz (η = 0.6) has gain of approximately:

8. The thermal noise floor in dBm is:

9. Doubling the bandwidth of a link (with everything else fixed) changes the noise floor by:

10. FSPL at 14 GHz over 15 km is approximately:

11. GEO satellite links overcome ~200 dB path loss primarily via:

12. The standard remedy for flat multipath fading on a microwave hop is:

15. References & Further Reading

  1. Rappaport, T. S. — Wireless Communications: Principles and Practice, 2nd ed. (two-ray, fading, Hata).
  2. Stutzman, W. L. & Thiele, G. A. — Antenna Theory and Design (dish gain, patterns).
  3. Kraus, J. D. & Marhefka, R. J. — Antennas for All Applications.
  4. ITU-R P.1546 / P.1812 — Point-to-area field-strength prediction methods.
  5. ITU-R P.838 — Specific attenuation model for rain.
  6. ITU-R P.618 — Propagation data and prediction methods for Earth–space telecommunication systems.
  7. Freeman, R. L. — Radio System Design for Telecommunications (microwave link engineering).

Prepared for ECE 523E — Antenna & Radio Wave Propagation, Department of Electrical & Communication Engineering, Masinde Muliro University of Science and Technology.