Module 05 / RF Fundamentals

Noise

A receiver never sees signal alone. Learn to move from random voltage and power density to a defensible weak-signal decision—through bandwidth, temperature, noise figure, stage order, interference, oscillator purity, and the measurement settings that shape what you see.

01 / 12

Noise sets the weak-signal limit

A −88.5 dBm available signal reaches a named receiver input at 2.45 GHz. Is it detectable?

Not enough information. The power level and carrier frequency do not determine a decision. We still need the source or antenna noise temperature, noise-density convention, equivalent noise bandwidth, receiver-added noise, in-channel interference and blockers, oscillator phase noise, a detection criterion, and assurance that every quantity uses the same reference plane.

  • −88.5 dBm signal
  • source N₀
  • Bₑₙᵦw
  • receiver F or Tₑ
  • I and criterion

The −88.5 dBm value is a new supplied receiver-input value. It is deliberately notderived from the +10 dBm EIRP example in Fields & Waves. Connecting those two values would require the missing propagation, antenna, polarization, mismatch, and loss terms.

Detectability is a conditional engineering statement

A signal can be below the integrated noise yet recoverable by coherent processing, or above it yet unusable because of interference, fading, distortion, or an unsuitable detector. “Above the noise floor” is not a complete requirement.

02 / 12

Random signals have measurable structure

If a noise waveform cannot be predicted sample by sample, what can an engineer measure repeatably?

A realization is one finite record from a random process. Its sample mean, RMS, variance, amplitude distribution, autocorrelation, and power spectral density are estimators—not promises that the next record will look the same. Longer records improve frequency resolution; independent averaging reduces estimator variation.

x(t)=s(t)+n(t)μn=E[n]x(t) = s(t) + n(t) \qquad \mu _{n} = E[n]σn2=E[(nμn)2]nrms=E[n2]\begin{aligned}\sigma_n^2&=\mathrm E[(n-\mu_n)^2]\\n_{\mathrm{rms}}&=\sqrt{\mathrm E[n^2]}\end{aligned}uncorrelated sources:σtotal2=σi2\text{uncorrelated sources}: \sigma _{\mathrm{total}}^{2} = \sum \sigma _{i}^{2}For zero-mean noise, RMS equals standard deviation—not zero. Correlated sources require covariance or cross-spectral terms.

Power spectral density carries squared-amplitude per hertz, such as V²/Hz. Amplitude spectral density is its square root, such as V/√Hz. Integrate PSD—not ASD—over the weighted bandwidth to obtain mean-square noise, then take a square root if an RMS amplitude is required.

Interactive · realization, distribution, spectrum

Random-noise laboratory

Step between repeatable finite records. The waveform changes; its estimated statistics and spectrum become more stable only with more samples and independent averages.

Prediction: what happens to a noisy PSD estimate when more independent records are averaged?
Noise model
Realization seed
2718
Sample mean
-0.0118
Sample RMS
0.9571
Sample variance
0.9159

μ̂ = (1/N)Σxᵢ · RMS = √[(1/N)Σxᵢ²] · σ̂² = (1/N)Σ(xᵢ − μ̂)²Normalized amplitude units. For zero-mean noise, RMS equals standard deviation. Uncorrelated source variances add; correlated sources require covariance or cross-spectral terms.

Model boundary: synthetic, finite, discrete-time, Nyquist-band-limited model. “White” describes the modeled spectrum, while “Gaussian” describes the amplitude distribution; neither implies physically infinite bandwidth or power.

Common misconceptionWhite noise means Gaussian noise.

White describes a flat spectral density over a stated band. Gaussian describes an amplitude probability distribution. A model may be one without the other, and no physical source is white over infinite bandwidth.

03 / 12

From noise density to noise power

Why does a flat −174 dBm/Hz source not produce −174 dBm on a 20 MHz power measurement?

Density is power per unit bandwidth. A linear filter weights that density, and total noise is its area after the filter. For a flat one-sided input density N₀ and a response normalized to unity peak gain, equivalent noise bandwidth replaces the real filter with an equal-area rectangle.

N=0Sn(f)H(f)2dfN=\int_0^\infty S_n(f)|H(f)|^2\,\mathrm dfBENBW=0H(f)2dfHmax2B_{\mathrm{ENBW}}=\frac{\int_0^\infty|H(f)|^2\,\mathrm df}{|H|_{\max}^2}Flat N0:N=N0BENBWN[dBm]=N0[dBm/Hz]+10log10(BENBW1Hz)\begin{aligned}\text{Flat }N_0:\quad N&=N_0B_{\mathrm{ENBW}}\\N[\mathrm{dBm}]&=N_0[\mathrm{dBm/Hz}]+10\log_{10}\left(\frac{B_{\mathrm{ENBW}}}{1\,\mathrm{Hz}}\right)\end{aligned}This module consistently uses one-sided, positive-frequency RF noise density.
Think about itIf flat-noise bandwidth doubles while density stays fixed, what happens to noise power and RMS noise voltage?
Answer

Power doubles, increasing 3.0103 dB. RMS voltage rises by √2. Increasing bandwidth tenfold raises noise power by 10 dB.

Common misconceptionA filter’s 3 dB bandwidth is always its noise bandwidth.

Not generally. For a one-pole low-pass, the one-sided ENBW is (π/2)f₃dB. Filter shape matters because noise power depends on the whole squared-magnitude response.

04 / 12

Thermal noise and the −174 dBm/Hz reference

Which temperature and bandwidth are hidden inside the familiar “−174 dBm” shortcut?

In the classical matched-source regime, available thermal-noise density is kT W/Hz. The Boltzmann constant is exact: k = 1.380649 × 10⁻²³ J/K. At the standard noise temperature T₀ = 290 K, kT₀ = 4.0038821 × 10⁻²¹ W/Hz = −173.975187 dBm/Hz. At 300 K it is approximately −173.828 dBm/Hz. Neither should silently be called “room temperature” without naming T.

Interactive · kT, resistance, and ENBW

Thermal-noise and bandwidth explorer

Start with available noise-power density, integrate it through a filter, then choose the correct resistor voltage reference: open circuit or matched load.

Prediction: with flat density, what does 10× more ENBW do to integrated noise power?
Filter model
Voltage reference
Available density kT
4.003882e-21 W/Hz-173.975 dBm/Hz
Integrated available noise
80.08 fW-100.965 dBm
Open-circuit voltage density
894.9 pV/√Hz
Matched-load RMS voltage
2.001 µV
Rectangular width
20.00 MHz

N = ∫₀∞ Sₙ(f)|H(f)|²df = kTBₑₙᵦwFor the one-pole low-pass model, Bₑₙᵦw = (π/2)f₃dB. The plot uses a one-sided, positive-frequency density.

Reference matters: a resistor’s open-circuit density is √(4kTR) V/√Hz. A matched load receives half that voltage, one quarter the mean-square voltage, and exactly kT W/Hz of available power.

Sv=4kTR[V2/Hz]en=4kTR[V/Hz]\begin{aligned}S_v&=4kTR\quad[\mathrm{V^2/Hz}]\\e_n&=\sqrt{4kTR}\quad[\mathrm{V/\sqrt{Hz}}]\end{aligned}vn,oc=4kTRBvn,matched=kTRBv_{n,\mathrm{oc}}=\sqrt{4kTRB}\qquad v_{n,\mathrm{matched}}=\sqrt{kTRB}R=50Ω,T=290K,B=20MHz:Pn=80.0776fW=100.9649dBmR = 50 \Omega , T = 290 K, B = 20 \mathrm{MHz}: P_{n} = 80.0776 \mathrm{fW} = -100.9649 \mathrm{dBm}Open-circuit density is 0.894861 nV/√Hz; matched-load density is 0.447431 nV/√Hz. The corresponding RMS values are 4.00194 µV and 2.00097 µV.

The factor of four is not missing power. A Thevenin source and equal load form a 2:1 voltage divider, so the load sees half the open-circuit voltage and one quarter the mean-square voltage. That voltage across R delivers kTB of available noise power.

Go deeperWhere the classical kT approximation stops being universal

Planck’s law replaces the classical approximation when hf is no longer much smaller than kT. At 2.45 GHz, hf/k ≈ 0.1176 K and hf/(kT) ≈ 4.05 × 10⁻⁴ at 290 K, so kTB is excellent here. It is not universal at cryogenic temperature or sufficiently high frequency.

05 / 12

Noise sources leave different fingerprints

Does every irregular spectrum belong in the same kTB calculation?

No. Source physics shapes spectrum, amplitude distribution, correlation, direction, time behavior, and mitigation. Thermal and ideal shot noise can be broadband; flicker grows close to low offset; burst noise is intermittent; the antenna collects a changing brightness scene; spurs and other transmitters can be deterministic.

Classify the mechanism before selecting a model
SourcePhysical or system originFingerprint and caveat
ThermalRandom carrier motion in resistive lossNearly white across ordinary RF bandwidths; scales with temperature
ShotDiscrete charge crossing a barrierOne-sided Sᵢ = 2qI A²/Hz for the ideal Poisson model
FlickerDevice and material processesRises toward low offset frequency; often described as 1/f-like
Burst / popcornDiscrete device-state changesTime-domain steps or pulses; non-Gaussian and nonstationary
AtmosphereOxygen, water vapor, rain, and other propagation mediaFrequency-, elevation-, weather-, and path-dependent brightness
Galactic / celestialSky brightness and discrete radio sourcesStrongly depends on frequency, direction, beam, and polarization
Ground / objectsThermal radiation coupled through the antenna patternOften warm, directional, and installation-dependent
Man-madeTransmitters, electronics, machinery, and infrastructureMay be impulsive, narrowband, broadband, periodic, or intermittent
QuantizationMapping a continuous input to discrete converter codesCan resemble white noise only under stated signal and decorrelation conditions
Spurs / interferenceDeterministic leakage or other emittersLines or occupied signals—not automatically random noise
One-sided shot noise:Si=2qI[A2/Hz]in=2qI[A/Hz]\begin{aligned}\text{One-sided shot noise:}\quad S_i&=2qI\quad[\mathrm{A^2/Hz}]\\i_n&=\sqrt{2qI}\quad[\mathrm{A/\sqrt{Hz}}]\end{aligned}q = 1.602176634 × 10⁻¹⁹ C exactly. Device bandwidth, excess noise, correlations, operating point, and a non-unity Fano factor may change the practical model.
Common misconceptionQuantization error is always independent white noise with Δ²/12 variance.

That approximation needs sufficient code activity and decorrelation. A coherent or low-level input can produce deterministic, signal-correlated error and spurs; clipping and nonlinearity are different failure modes again.

06 / 12

Phase noise is not an additive broadband floor

Why can a strong signal outside the channel raise in-channel noise even when the RF filter rejects its carrier?

A real oscillator’s phase fluctuates. Mixing a blocker with the local oscillator’s noise sidebands can translate energy into the wanted channel: reciprocal mixing. This impairment depends on blocker power, frequency offset, local-oscillator phase-noise density, filtering, and mixer behavior—not only on the receiver’s additive noise figure.

Interactive · additive noise, modulation noise, and spurs

Additive and phase-noise explorer

Scrub a slowed, normalized carrier phasor and compare mechanisms that can look similar on a spectrum display but require different models.

Prediction: which mechanism lets a strong adjacent blocker raise in-channel noise through reciprocal mixing?
Disturbance model
Example carrier
-20 dBm at 2.45 GHz
Example SSB phase-noise density
-100 dBc/Hzat 100 kHz offset, in a 1 Hz bandwidth
Small-noise sideband estimate
-120 dBm/Hz-20 dBm + (-100 dBc/Hz)

v(t) = A[1 + a(t)]cos(2πfᶜt + φₙ(t)) + nₐ(t)Illustrative normalized geometry, not a calibrated oscillator simulation. L(fₒffₛₑₜ) is a single-sideband density ratio to a named carrier power, carrier frequency, offset, and 1 Hz bandwidth.

Single-sideband phase noise L(foffset) in dBc/Hz is incomplete unless the carrier frequency and power, offset frequency, 1 Hz normalization, sideband convention, and measurement conditions are stated. In the small-noise direct-spectrum approximation, an absolute sideband density is the carrier level in dBm plus L in dBc/Hz.

Common misconceptionA low receiver noise figure guarantees good blocker performance.

NF describes small-signal SNR degradation under stated source conditions. Reciprocal mixing, compression, intermodulation, desensitization, and ADC range can dominate in the presence of strong signals.

07 / 12

What a spectrum analyzer actually displays

When the displayed trace falls after you narrow RBW or VBW, did the source become quieter?

The analyzer passes input through a resolution filter, detects the result, and estimates a display value. RBW sets RF resolution and the noise collected per bin; its true ENBW depends on filter shape. VBW smooths detected display values. Trace averaging reduces estimator variation. Sample, RMS, average, and peak detectors answer different statistical questions, while linear-power and logarithmic averaging are not interchangeable. Neither VBW nor averaging changes the source PSD.

Interactive · density, bins, and display statistics

Spectrum-analyzer noise explorer

Separate the input density from noise collected in one resolution-filter bin, the analyzer’s own input-referred noise, and the final displayed estimate.

Prediction: when RBW increases 10× for flat input noise, what rises by about 10 dB?
Resolution-filter model
Detector definition in this model
Illustrative 15 dB preamplifier
  • Displayed estimate
  • Input source per bin
  • Instrument floor per bin
Input noise density
-160 dBm/Hz
Filter ENBW
10.60 kHz
Source noise / bin
-119.75 dBm
Instrument floor / bin
-119.75 dBm
Approximate observation time
64.8 ms

Pbin = PSD + 10log₁₀(Bₑₙᵦw/1 Hz); powers from source and instrument add in wattsRMS = mean of 8 linear-power samples, sample = 1 sample, and positive peak = maximum of exactly 8 samples. Trace averaging is then performed in linear power; VBW is modeled as a moving average.

Educational model, not a calibrated instrument: the assumed input-referred instrument density is −170 dBm/Hz at 0 dB attenuation, and the illustrative preamp lowers it 15 dB. Real DANL, ENBW, detector behavior, and sweep time are model- and setting-specific. VBW and averaging reduce display variation; they do not reduce the source PSD or change RF resolution.

Displayed average noise level is a settings-specific instrument quantity, not a universal physical floor. More input attenuation protects against overload but normally raises the input-referred analyzer floor. A preamplifier can lower that floor while reducing headroom. Narrower RBW collects less flat noise per bin and generally requires more acquisition time.

Go deeperSubtracting signal and noise in linear power

If a signal-plus-noise measurement is only 1 dB above a separate equal-bandwidth noise measurement, linear subtraction gives signal/noise = 10^(1/10) − 1 = 0.2589. The signal alone is therefore about 5.87 dB below the noise—not 1 dB above it. This requires stable, comparable measurements and uncorrelated added powers.

Common misconceptionEvery noise trace needs a universal 2.51 dB correction.

Corrections depend on the analyzer architecture, detector, averaging domain, logarithmic processing, filter shape, and the quantity being reported. Use the instrument’s documented noise-marker method and uncertainty, not a memorized universal offset.

08 / 12

SNR, C/N, C/N₀, and SINR

Which ratio still makes sense before a receiver bandwidth has been chosen?

C/N₀ compares carrier power to noise-power density and therefore carries the logarithmic unit dB-Hz. It does not become the dimensionless in-band C/N until a bandwidth is specified. Use “carrier” only for a clearly identified carrier; otherwise SNR is the safer general label.

SNR=PsPnSINR=PsPn+Pi\mathrm{SNR} = \frac{P_{s}}{P_{n}} \qquad \mathrm{SINR} = \frac{P_{s}}{P_{n} + P_{i}}CN0[dBHz]=C[dBm]N0[dBmHz]\frac{C}{N_{0}} [\mathrm{dB}-\mathrm{Hz}] = C[\mathrm{dBm}] - N_{0}[\frac{\mathrm{dBm}}{\mathrm{Hz}}]CN [dB]=CN0 [dB ⁣ ⁣Hz]10log10(B1Hz)\frac CN\ [\mathrm{dB}]=\frac C{N_0}\ [\mathrm{dB\!\cdot\!Hz}]-10\log_{10}\left(\frac B{1\,\mathrm{Hz}}\right)dB-Hz is not an ordinary dimensionless dB ratio; the “Hz” records the density normalization.

Each numerator and denominator must share a reference plane, bandwidth, and averaging definition. Add independent noise and interference in watts before taking a ratio. As a later digital-link preview, Eb/N₀ = (C/N₀)/Rb only after the information-bit rate and consistent reference definitions are known.

Common misconceptionC/N and C/N₀ are interchangeable because both are reported in decibels.

C/N is bandwidth-dependent. C/N₀ is a density ratio in dB-Hz. Confusing them silently discards the 10log₁₀(B/1 Hz) term.

09 / 12

Noise factor, noise figure, and equivalent temperature

How can one receiver be described by either a dimensionless factor or a temperature in kelvin?

Noise factor is the degradation of available signal-to-noise ratio through a two-port under stated source and reference conditions. Noise figure is that same factor in decibels. Equivalent input noise temperature represents the receiver’s added noise at its input plane.

F=SNRinSNRoutNF=10log10FF = \frac{\mathrm{SNR}_{\mathrm{in}}}{\mathrm{SNR}_{\mathrm{out}}} \qquad \mathrm{NF} = 10\log _{10}FTe=T0(F1)F=1+TeT0T0=290KT_{e} = T_{0}(F - 1) \qquad F = 1 + \frac{T_{e}}{T_{0}} \qquad T_{0} = 290 KNout=GkB(Ts+Te)N_{\mathrm{out}} = G k B(T_{s} + T_{e})G is available power gain and every temperature is referred to the same input plane.

A matched passive loss L at physical temperature Tp has G = 1/L, Tₑ = (L − 1)Tp, and F = 1 + (L − 1)Tp/T₀. Only when Tp = T₀ does F = L and noise figure equal loss in decibels.

Go deeperY-factor measurement in one line

With calibrated hot and cold source temperatures at the same input plane, Y = Phot/Pcold = (Thot + Tₑ)/(Tcold + Tₑ), so Tₑ = (Thot − YTcold)/(Y − 1). Real measurements must account for source ENR, mismatch, loss, bandwidth, gain stability, linearity, and uncertainty.

Common misconceptionA 2 dB noise figure means the receiver adds a fixed −172 dBm/Hz floor.

NF is a ratio tied to T₀ and reference conditions, not an absolute output floor. Gain, source temperature, bandwidth, losses, impedance conditions, and reference plane still matter.

10 / 12

Why receiver stage order matters

Can the same LNA, filter, and IF amplifier have different total noise figure when their order changes?

Yes. Friis’ equation discounts a stage’s excess noise by all preceding power gain. That makes early low-noise gain powerful and early passive loss expensive. Convert every dB value to linear G and F before applying Friis; never add stage noise figures in decibels.

Interactive · Friis equation in linear units

Cascade-noise explorer

Reorder the same three stages and watch early gain suppress later noise contributions. Add cable loss only at the named input reference plane.

Prediction: which matters more here—removing 1 dB before the LNA or improving NF after substantial gain?
All Friis calculations use power gain G and noise factor F in linear units
Order / stageGainNF / FFriis contributionCumulative gainReorder
1. LNA15.0 dB / 31.6231.5 dB / 1.41251.41253815.0 dB
2. Passive filter (290 K)-3.0 dB / 0.5013.0 dB / 1.99530.03147312.0 dB
3. IF amplifier30.0 dB / 1000.0005.0 dB / 3.16230.13643042.0 dB
Total power gain
42.000 dB1.5849e+4 linear
Total noise factor
1.580441
Total noise figure
1.9878 dB
Equivalent input noise temperature
168.328 K

Ftotal = F₁ + (F₂ − 1)/G₁ + (F₃ − 1)/(G₁G₂) + …At 290 K, matched passive loss L has G = 1/L and F = L. The initial LNA–filter–IF order gives F = 1.580441, NF = 1.987783 dB, and Tₑ = 168.328 K.

Noise is not the only ordering constraint. A preselector ahead of the LNA may be essential for blocker rejection, stability, linearity, image rejection, or protection even when it worsens small-signal NF. The quietest Friis order is not automatically a buildable receiver.

For the initial +15 dB/NF 1.5 dB LNA, −3 dB/NF 3 dB filter at 290 K, and +30 dB/NF 5 dB IF amplifier, the three Friis contributions are 1.412538, 0.031473, and 0.136430. Total gain is 42 dB, F = 1.580441, NF = 1.987783 dB, and Tₑ = 168.328 K. Moving the filter ahead of the LNA gives F = 2.954813, NF = 4.705301 dB, and Tₑ = 566.896 K.

11 / 12

Antenna temperature and receiver sensitivity

Is antenna temperature the temperature of the antenna metal, the weather, or the sky?

It is an equivalent noise temperature derived from the brightness-temperature scene weighted by the receiving antenna’s directional, polarization-sensitive pattern, plus applicable antenna losses. It varies with frequency, pointing, environment, atmosphere, ground, nearby objects, and polarization. It is not automatically 290 K, 3 K, or 4 K.

Ta=Tb(θ,ϕ)Gr(θ,ϕ)dΩGr(θ,ϕ)dΩT_a=\frac{\iint T_b(\theta,\phi)G_r(\theta,\phi)\,\mathrm d\Omega}{\iint G_r(\theta,\phi)\,\mathrm d\Omega}Tsys=Ta+TeT_{\mathrm{sys}} = T_{a} + T_{e}290Kconvention:sensitivity=173.9752+10log10(B1Hz)+NF+SNRrequired290 K \mathrm{convention}: \text{sensitivity} = -173.9752 + 10\log _{10}(\frac{B}{1 \mathrm{Hz}}) + \mathrm{NF} + \mathrm{SNR}_{\mathrm{required}}Tsys addition is valid only when Tₐ and Tₑ are referred to the same plane. The antenna integral shown is a simplified single-polarization form.
Interactive · common-plane system noise and threshold

Receiver margin explorer

Choose either the conventional 290 K noise-figure method or an actual antenna temperature plus equivalent receiver temperature. Never add NF in decibels directly to a non-290 K source.

Temperature model at the named receiver input plane
In-channel interference at this same reference plane
Decision at the receiver input

Passes the entered criterion

The 10.0 dB criterion is an explicit hypothetical requirement, not a universal definition of detectability. Coding, integration time, false-alarm probability, fading, and implementation loss can move the real threshold.

Reference-plane model

Standard 290 K source + 168.3 K receiver

All source and receiver temperatures are referred to the plane ahead of the selected cable loss.

Source noise density
-173.9752 dBm/Hz
Receiver NF / Tₑ at input plane
1.9878 dB168.328 K
System temperature
458.328 K
Total noise density
-171.9874 dBm/Hz
Integrated noise
-98.9771 dBm
C/N₀
83.4874 dB-Hz
C/N
10.4771 dB
Conditional sensitivity
-88.9771 dBm
Margin
+0.4771 dB
Frequency check
2.45 GHzclassical kT model selected
Noise power
126.6 fW

N = kT₀BF; sensitivity = N[dBm] + required C/NC/N₀ = C − N₀ in dB-Hz. C/N = C/N₀ − 10log₁₀(B/1 Hz). Powers, not decibel values, are added when interference is included.

Explore a deliberately simple sky-and-ground antenna-temperature model

This is a hypothetical two-region weighting exercise, not a sky map or antenna simulator. It assumes a lossless normalized pattern, 0.65 of pattern weight on a 30 K sky region and 0.35 on a 290 K ground region, giving Tₐ = 121.0 K.

Real Tₐ is a pattern-weighted brightness-temperature integral over direction, polarization, frequency, atmosphere, ground, objects, antenna loss, and pointing. It is not the metal temperature and is not automatically 290 K or the cosmic-background temperature.

When Tₐ differs from 290 K, convert receiver NF to Tₑ and use kB(Tₐ + Tₑ). The conventional sensitivity equation is otherwise liable to hide a warm ground contribution, a cold-sky advantage, or loss between the antenna and receiver. A quoted “sensitivity” must also state its bandwidth, criterion, probability or error target, and implementation assumptions.

12 / 12

Putting it together: one 2.45 GHz noise journey

Under one explicit set of assumptions, does the supplied −88.5 dBm signal meet a 10 dB in-band requirement?

Assume the available signal and antenna noise are referred to the receiver input; Tₐ = 290 K; one-sided density and Bₑₙᵦw = 20 MHz are used; the LNA–filter–IF chain is in its initial order; and there is no in-channel interference, reciprocal mixing, compression, fading, or implementation loss. The 10 dB requirement is hypothetical but explicit.

Common-plane calculation from source density to conditional margin
StepValueMeaning
Available signal−88.5000 dBmSupplied at the receiver input; not derived from the prior module’s +10 dBm EIRP
SourceTₐ = 290 KN₀ = −173.9752 dBm/Hz at the same reference plane
Channel2.45 GHz; Bₑₙᵦw = 20 MHzSource noise = −100.9649 dBm
ReceiverG = 42 dB; F = 1.580441NF = 1.9878 dB; Tₑ = 168.328 K
SystemTsys = 458.328 KInput-referred density = −171.9874 dBm/Hz; noise = −98.9771 dBm
RatiosC/N₀ = 83.4874 dB-HzC/N = 10.4771 dB in 20 MHz
10 dB criterionSensitivity = −88.9771 dBmMargin = +0.4771 dB: conditional pass
Receiver outputSignal = −46.5000 dBmNoise = −56.9771 dBm; SNR remains 10.4771 dB
C/N=88.5000(98.9771)=10.4771dBC/N=-88.5000-(-98.9771)=10.4771\,\mathrm{dB}margin=88.5000(88.9771)=+0.4771dB\mathrm{margin} = -88.5000 - (-88.9771) = +0.4771 \mathrm{dB}Conditional answer: yes, narrowly, under only the assumptions above.

Now place a matched 1 dB cable at 290 K ahead of the LNA and move the reference plane ahead of that cable. The complete network NF becomes 2.9878 dB—exactly 1 dB worse—while receiver Tₑ becomes 287.001 K and Tsys becomes 577.001 K. Input-referred noise becomes −97.9771 dBm, C/N becomes 9.4771 dB, sensitivity becomes −87.9771 dBm, and margin becomes −0.5229 dB: a conditional fail.

The connected receiver-noise model

Classify the source. State the density convention and reference plane. Integrate with ENBW. Refer source and receiver temperatures to one plane. Cascade linear factors in order. Add independent powers in watts. Then compare the resulting SNR or SINR with a named criterion.

Ungraded review

Check your understanding

Answer each question in your own words, then reveal the model answer.

  1. 01What thermal-noise power does −173.9752 dBm/Hz produce across a 20 MHz equivalent noise bandwidth?
    Model answer

    −100.9649 dBm at 290 K. Doubling the bandwidth would raise total noise by 3.0103 dB and RMS noise voltage by √2.

  2. 02Why does placing a passive filter before an LNA usually worsen receiver noise performance?
    Model answer

    Friis’ equation discounts later excess noise by preceding gain. Early passive loss receives no such protection: in the lesson’s chain, filter-first ordering raises NF from about 1.99 dB to 4.71 dB.

  3. 03A −88.5 dBm signal faces −98.9771 dBm of input-referred noise and requires 10 dB C/N. Does it pass?
    Model answer

    Yes, narrowly: C/N is 10.4771 dB and margin is +0.4771 dB. A matched 1 dB cable ahead of the LNA changes that margin to −0.5229 dB under the stated 290 K assumptions.

Sources and further study

NIST fixes the exact constants; MIT, ITU-R, and IEEE provide theory and terminology; Keysight and Rohde & Schwarz document receiver and instrument practice. Manufacturer-specific behavior should always be checked against the exact instrument manual and settings.

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