Wireless Notes
Learn satellite link design with uplink downlink budget calculation, C/N carrier to noise, G/T figure of merit, rain attenuation Ku Ka band, link margin, and design examples for engineering students.
A complete guide to satellite link design covering link budget calculations, carrier-to-noise ratio analysis, rain attenuation effects, system margin, and practical design considerations for reliable satellite communication links.
Link Budget Fundamentals
The Basic Link Equation
The received signal power at any point in a communication link is:
P_received (dBW) = EIRP + G_receive - L_total
Where:
- EIRP = Effective Isotropic Radiated Power (transmitter power + antenna gain)
- G_receive = Receive antenna gain
- L_total = Total losses (free-space path loss + atmospheric + rain + pointing + miscellaneous)
Expanding the EIRP: EIRP (dBW) = P_transmitter (dBW) + G_transmit (dBi) - L_feed (dB)
Complete Link Budget Table
A typical Ku-band satellite downlink budget:
| Parameter | Symbol | Value | Unit |
|---|---|---|---|
| Satellite transmit power | P_t | 10 | dBW |
| Satellite antenna gain | G_t | 36 | dBi |
| Satellite feed loss | L_feed | -1 | dB |
| EIRP | 45 | dBW | |
| Free-space path loss (12 GHz, 37,500 km) | L_fs | -205.8 | dB |
| Atmospheric absorption | L_atm | -0.3 | dB |
| Rain attenuation (99.9% availability) | L_rain | -3.0 | dB |
| Pointing loss | L_point | -0.5 | dB |
| Polarization mismatch | L_pol | -0.3 | dB |
| Total path loss | -209.9 | dB | |
| Receive antenna gain (1.2m dish) | G_r | 44.5 | dBi |
| Receive feed loss | L_rx_feed | -0.5 | dB |
| Received power | P_r | -120.9 | dBW |
Free-Space Path Loss
The Inverse Square Law
Free-space path loss (FSPL) is the dominant loss in any satellite link. It represents the spreading of energy over an ever-larger sphere as the wave propagates:
FSPL (dB) = 20×log₁₀(4πd/λ) = 20×log₁₀(4πdf/c)
Where d = distance (m), f = frequency (Hz), c = speed of light
Simplified: FSPL (dB) = 92.45 + 20×log₁₀(f_GHz) + 20×log₁₀(d_km)
| Orbit | Distance | FSPL at C-band (4 GHz) | FSPL at Ku-band (12 GHz) | FSPL at Ka-band (20 GHz) |
|---|---|---|---|---|
| LEO (600 km) | 600 km | 168.0 dB | 177.5 dB | 181.9 dB |
| MEO (8,000 km) | 8,000 km | 190.5 dB | 200.0 dB | 204.5 dB |
| GEO (35,786 km) | 37,500 km* | 196.5 dB | 205.8 dB | 210.3 dB |
*Slant range varies with elevation angle; 37,500 km is typical at 30° elevation.
The path loss increases 6 dB for every doubling of distance and 6 dB for every doubling of frequency. This is why GEO satellites operating at Ka-band face the greatest path loss challenge (~210 dB).
Carrier-to-Noise Ratio (C/N)
System Noise Temperature
The receiver's ability to detect the signal depends on the carrier-to-noise ratio (C/N). The noise power is determined by the system noise temperature:
N = k × T_system × B
Where k = Boltzmann's constant (−228.6 dBW/K/Hz), T_system = total system noise temperature (K), B = bandwidth (Hz)
The system noise temperature includes contributions from:
| Source | Typical Temp | Notes |
|---|---|---|
| Antenna noise (sky temp) | 20-50 K | Higher at low elevation, rain |
| Feed/waveguide loss | 10-30 K | T_feed = (L-1) × T_physical |
| LNA noise figure | 40-100 K | Quality of low-noise amplifier |
| Total T_system | 80-200 K | Sum of all contributions |
C/N Calculation
C/N (dB) = P_received - N = P_received - (k + T_system + B)
C/N = EIRP + G/T - FSPL - L_other - k - B
Where G/T is the receiver figure of merit (antenna gain divided by system noise temperature, in dB/K).
The G/T is the single most important specification of a satellite earth station receiver — it captures both the antenna's ability to collect signal (G) and the system's resistance to noise (1/T) in one number.
Rain Fade Analysis
How Rain Affects Satellite Links
Rain is the most significant variable propagation loss for satellite links above 10 GHz. Raindrops absorb and scatter microwave energy, with attenuation increasing sharply with frequency:
| Frequency | Rain attenuation (25 mm/hr rain, 5 km path) |
|---|---|
| 4 GHz (C-band) | 0.1 dB (negligible) |
| 12 GHz (Ku-band) | 4-6 dB |
| 20 GHz (Ka-band) | 10-15 dB |
| 30 GHz (Ka uplink) | 18-25 dB |
This is why C-band is preferred in tropical regions like Southeast Asia and Sub-Saharan Africa where heavy rainfall is frequent. Ka-band systems must include significant rain margin or use adaptive techniques.
ITU-R Rain Model
The ITU-R P.618 recommendation provides the standard method for calculating rain attenuation:
- Determine rain climate zone (A-Q) based on geographic location
- Look up the rain rate exceeded for the desired availability (e.g., R₀.₀₁ = rain rate exceeded 0.01% of time)
- Calculate effective rain path length considering rain height and elevation angle
- Apply specific attenuation coefficient (γ_R) based on frequency and polarization
For example, in Mumbai (rain zone M, R₀.₀₁ = 63 mm/hr), a 12 GHz link at 60° elevation experiences approximately 8 dB rain fade for 99.99% availability.
Rain Fade Mitigation Techniques
| Technique | Description | Complexity |
|---|---|---|
| Fixed margin | Design link with extra C/N to handle worst-case rain | Simple but wasteful |
| Adaptive coding and modulation (ACM) | Reduce data rate during rain (robust modulation) | Complex, efficient |
| Site diversity | Two earth stations 20+ km apart (rarely rains at both simultaneously) | Expensive |
| Uplink power control | Increase transmitter power when rain is detected | Moderate |
| Frequency scaling | Measure attenuation at beacon frequency, predict for traffic frequency | Moderate |
End-to-End Link Design
Uplink and Downlink Separation
A complete satellite link has two segments:
Uplink: Earth Station → Satellite (e.g., 14 GHz) Downlink: Satellite → Earth Station (e.g., 12 GHz)
Each segment has its own C/N ratio. The overall end-to-end C/N is:
(C/N)_total⁻¹ = (C/N)_uplink⁻¹ + (C/N)_downlink⁻¹ + (C/I)_interference⁻¹
This means the weakest link dominates. If the uplink C/N is 20 dB and the downlink is 14 dB, the total is approximately 13.7 dB (dominated by the poorer downlink).
Design Margin
Engineers include margin above the minimum required C/N to account for:
| Margin Component | Typical Value |
|---|---|
| Rain fade (99.9% availability) | 3-8 dB |
| Satellite aging (power degradation) | 1-2 dB |
| Antenna pointing errors | 0.3-1 dB |
| Equipment degradation | 0.5-1 dB |
| Implementation loss | 1-2 dB |
| Total design margin | 6-14 dB |
Practical Link Budget Example
Design a DTH (Direct-to-Home) TV downlink:
Requirements: QPSK modulation, FEC rate 3/4, required C/N = 7.8 dB for quasi-error-free reception
| Parameter | Value |
|---|---|
| Satellite EIRP per carrier | 52 dBW |
| Frequency | 12.5 GHz |
| Slant range | 38,000 km |
| Free-space loss | -206.0 dB |
| Atmospheric loss | -0.3 dB |
| Rain margin (99.7%) | -2.0 dB |
| Receive antenna (60 cm dish) | 37.5 dBi |
| System noise temperature | 140 K (21.5 dBK) |
| Carrier bandwidth | 36 MHz (75.6 dBHz) |
| Received C/N | 10.8 dB |
| Required C/N | 7.8 dB |
| Margin | 3.0 dB ✓ |
The 3 dB margin means the link will work reliably until rain fade exceeds the allocated 2 dB rain margin, at which point the picture may freeze momentarily.
Key Takeaways
- Link budget analysis tracks signal power from transmitter to receiver, accounting for all gains (antennas) and losses (path loss, atmosphere, rain) in decibels
- Free-space path loss exceeds 200 dB for GEO satellites and increases 6 dB per doubling of either distance or frequency
- G/T (receiver figure of merit) combines antenna gain and noise temperature into one number that characterizes receive station quality
- Rain attenuation is the dominant variable loss above 10 GHz, increasing dramatically with frequency (negligible at C-band, severe at Ka-band)
- The overall link C/N is dominated by the weakest segment (uplink or downlink) — both must be designed with adequate margin
- Adaptive coding and modulation (ACM) is the most bandwidth-efficient rain fade mitigation technique, trading data rate for robustness during rain events
- A well-designed satellite link includes 6-14 dB total margin to ensure reliable operation across seasonal, weather, and equipment aging variations
Exam Focus
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