The specific
intensity $I_\nu$ of radiation is defined by
$$I_\nu \equiv {dP \over (\cos \theta d \sigma) d \nu d
\Omega}\rlap{\quad
\href{Brightness.html#SpecificIntensity}{\rm {(2A1)}}}$$
where $dP$ is the power received
by a detector with projected area $(\cos \theta d \sigma)$ in the solid
angle $d
\Omega$ and in the frequency range $\nu$ to $\nu + d\nu$. The mks
units of $I_\nu$ are W
m$^{-2}$ Hz$^{-1}$ sr$^{-1}$. Specific intensity is
conserved (is constant) along
any ray in empty space. It is a property of the source only,
independent of the distance between the source and the observer.

The
linear
absorption coefficient
at frequency $\nu$ of an absorber is defined as $$\kappa_\nu \equiv
{dp_\nu \over ds}\rlap{\quad
\href{Radxfer.html#KappaNu}{\rm {(2B1)}}}$$
The optical
depth $\tau_\nu$
at frequency $\nu$ is defined as
$$\tau_\nu \equiv \int_{s_{\rm
out}}^{s_{\rm in}} -\kappa_\nu(s') ds'\rlap{\quad
\href{Radxfer.html#Opacity}{\rm {(2B2)}}}
$$
The emission
coefficient is
defined as
$$\epsilon_\nu \equiv {dI_\nu \over
ds}\rlap{\quad
\href{Radxfer.html#EmissionCoefficient}{\rm {(2B3)}}}$$
The equation
of radiative transfer
is
$${d I_\nu \over ds} = -\kappa_\nu
I_\nu + \epsilon_\nu\rlap{\quad
\href{Radxfer.html#RadXferEq}{\rm {(2B4)}}}$$
In Local Thermodyamic Equilibrium (LTE), Kirchoff's
law states that
$${\epsilon_\nu \over \kappa_\nu} = B_\nu(T)\rlap{\quad
\href{Radxfer.html#KirchoffsLaw}{\rm {(2B5)}}}$$
The brightness
temperature of
a source with any specific
intensity $I_\nu$ is defined as
$$T_{\rm b}(\nu) \equiv
{I_\nu c^2 \over 2 k \nu^2}\rlap{\quad
\href{Radxfer.html#BrightnessTemp}{\rm {(2B6)}}}$$
The Rayleigh-Jeans
approximation for
the specific intensity of blackbody radiation when $h \nu \ll kT$ is
$$B_\nu = {2 k T \nu^2 \over c^2}\rlap{\quad
\href{BlackBodyRad.html#RJlaw}{\rm {(2C2)}}}$$
Planck's
law for the specific
intensity of blackbody radiation is
$$B_\nu = {2 h \nu^3 \over c^2} {1 \over \exp\bigl({h \nu \over k
T}\bigr)
-1}\rlap{\quad \href{BlackBodyRad.html#PlanckLaw}{\rm {(2C3)}}}$$
The total
intensity of blackbody
radiation is:
$$B(T) \equiv \int_0^\infty B_\nu(T) d\nu = {\sigma
T^4 \over \pi}
\rlap{\quad \href{BlackBodyRad.html#IntBright}{\rm {(2C4)}}}$$
where the Stefan-Boltzmann
constant $\sigma$ is defined by
$$\sigma \equiv {2 \pi^5 k^4 \over 15 c^2 h^3} \approx 5.67 \times
10^{-5} {{\rm erg} \over {\rm cm}^2 {\rm ~s~K}^4 {\rm ~sr}}$$
The total
energy density of blackbody
radiation is
$$u = {4 \sigma T^4\over c}
\rlap{\quad \href{BlackBodyRad.html#BBEdensity}{\rm {(2C5)}}}$$
The Nyquist
formula approximating the spectral power generated by a warm
resistor in the limit $h \nu \ll k T$ is
$$P_\nu = k T
\rlap{\quad \href{BlackBodyRad.html#NyquistLaw}{\rm {(2C6)}}}$$
At any frequency, $$P_\nu
= {h \nu \over {\exp\bigl({h \nu \over kT}\bigr)
-1}}
\rlap{\quad \href{BlackBodyRad.html#QuantumNyquistLaw}{\rm {(2C7)}}}$$
$$E_\bot = {q \dot{v} \sin\theta \over
r c^2}\rlap{\quad \href{LarmorRad.html#LarmorEField}{\rm {(2D1)}}}$$
In a vacuum, the Poynting
flux, or
power per unit
area (erg s$^{-1}$ cm$^{-2}$), is
$$\vert \vec{S} \vert = {c \over 4 \pi}E^2\rlap{\quad
\href{LarmorRad.html#PoyntingFlux}{\rm {(2D2)}}}$$
The total power emitted by an accelerated charge is given by Larmor's
formula
$$P = {2 \over 3}{q^2 \dot{v}^2 \over c^3}\rlap{\quad
\href{LarmorRad.html#LarmorPower}{\rm {(2D3)}}}$$
valid only if $v \ll c$.

Radiation
resistance is defined by
$$R \equiv {2 \langle P \rangle \over
I_0^2}\rlap{\quad
\href{AntennaTheory.html#RadiationResistance}{\rm {(3A3)}}}$$
Energy conservation implies the
average power gain of a lossless antenna is
$$ \langle G \rangle = 1\rlap{\quad
\href{AntennaTheory.html#AverageGain}{\rm {(3A4)}}}$$
The effective
area of an antenna is defined by
$$ A_{\rm e} \equiv P_\nu / S_{\rm
(matched)}\rlap{\quad
\href{AntennaTheory.html#EffectiveArea}{\rm {(3A5)}}}$$
The average effective area of any lossless antenna is $$\langle A_{\rm e} \rangle = {\lambda^2 \over 4 \pi}\rlap{\quad \href{AntennaTheory.html#AverageArea}{\rm {(3A6)}}}$$
Reciprocity
implies
$$G(\theta, \phi) \propto
A_{\rm e}(\theta, \phi)\rlap{\quad
\href{AntennaTheory.html#Reciprocity}{\rm {(3A7)}}}$$
Reciprocity and energy conservation imply:
$$A_{\rm e}(\theta, \phi) = {\lambda^2
G(\theta, \phi) \over 4 \pi}\rlap{\quad
\href{AntennaTheory.html#GainArea}{\rm {(3A8)}}}$$
Antenna
temperature is defined by
$$T_{\rm A} \equiv {P_\nu \over k}\rlap{\quad
\href{AntennaTheory.html#AntennaTemp}{\rm {(3A9)}}}$$
Paraboloidal Reflectors:
$$z = {r^2 \over 4 f}~, ~f = {\rm ~focal~length}\rlap{\quadFar-field Distance:
$$ R_{\rm ff} \approx {D^2 \over 4
\lambda}\rlap{\quad
\href{ReflectorAntennas.html#FarField}{\rm {(3B2)}}}$$
Field pattern:
$$l \equiv \sin\theta\rlap{\quad$$u \equiv {x \over \lambda}\rlap{\quad
\href{ReflectorAntennas.html#DefineU}{\rm {(3B4)}}}$$
$$f(l) = \int_{\rm aperture} g(u) e^{-i 2 \pi l u} du \rlap{\quad
\href{ReflectorAntennas.html#FieldPattern}{\rm {(3B5)}}}$$
In the far field, the electric-field pattern of an aperture antenna is the Fourier transform of the electric field illuminating the aperture.
$$P(\theta) \propto {\rm sinc}^2
\biggl(
{\theta D \over \lambda} \biggr)\rlap{\quad
\href{ReflectorAntennas.html#PowerPattern}{\rm {(3B6)}}}$$

Two-dimensional
aperture field pattern:
$$f(l,m) \propto
\int_{-\infty}^{\infty} \int_{-\infty}^{\infty}
g(u,v) e^{-i 2 \pi(l u + mv)} d u d v \rlap{\quad
\href{2DApertures.html#2DFieldPattern}{\rm {(3C1)}}}$$
where $m$ is the $y$-axis analog of $l$ on the $x$-axis, and $v \equiv y / \lambda$.
The electric field pattern of a two-dimensional aperture is the two-dimensional Fourier transform of the aperture field illumination.$$\eta_{\rm
A} \equiv { {\rm max}(A_{\rm e}) \over
A_{\rm geom}}\rlap{\quad
\href{2DApertures.html#ApertureEfficiency}{\rm {(3C3)}}}$$
The half-power beamwidth (HPBW) for a
circular Gaussian illumination pattern is
The surface efficiency $\eta$ of a reflector whose surface errors $\epsilon$ have rms $\sigma$ is given by the Ruze equation:

Noise
temperature is defined by
The system
noise temperature is the sum of noise contributions from all
sources:
$$T_{\rm sys} = T_{\rm cmb} + \Delta
T_{\rm source} + T_{\rm atm} +
T_{\rm spillover} + T_{\rm rcvr} + \dots \rlap{\quad
\href{Radiometers.html#SystemNoise}{\rm {(3F2)}}}$$
$$\sigma_{\rm T} \approx T_{\rm sys}
\biggl[ {1 \over \Delta
\nu_{\rm RF} \tau}
\biggr]^{1/2}\rlap{\quad
\href{Radiometers.html#IdealRadiometer}{\rm {(3F3)}}}$$
The practical
total-power radiometer equation includes the effects of gain
fluctuations: $$\sigma_{\rm T} \approx T_{\rm sys}
\biggl[ {1 \over \Delta
\nu_{\rm RF} \tau} + \biggl( {\Delta G \over G} \biggr)^2
\biggr]^{1/2}\rlap{\quad
\href{Radiometers.html#Radiometer}{\rm {(3F4)}}}$$
The Dicke-switching
radiometer equation is
$$\sigma_{\rm T} \approx 2 T_{\rm
sys}\biggl[ { 1 \over \Delta \nu_{\rm RF} \tau} \biggr]^{1/2}\rlap{\quad
\href{Radiometers.html#DickeRadiometer}{\rm {(3F5)}}} $$

At frequencies low enough that
$\tau_\nu \gg 1$, the HII region becomes opaque, its spectrum
approaches that of a black body with temperature $T\
\sim 10^4$ K, and the flux density varies as $S \propto \nu^2$. At very
high frequencies, $\tau_\nu \ll 1$, the HII region is nearly
transparent, and
$$S_\nu \propto {2 k T \nu^2 \over c^2} \tau_\nu \propto \nu^{-0.1}$$
On a log-log plot, the overall spectrum of a uniform HII region looks
like this, with the spectral break corresponding to the frequency at
which $\tau_\nu \approx 1$:

The emission
measure of a plasma is defined by
$${ EM \over {\rm pc~cm}^{-6}} \equiv \int_{\rm los} \biggl( { N_{\rm e} \over {\rm cm}^{-3} } \biggr)^2 d \biggl( {s \over {\rm pc} } \biggr)\rlap{\quad \href{FreeFreeEmission.html#EmissionMeasure}{\rm {(4B5)}}}$$
The free-free
optical depth of a plasma is
$$\tau_\nu \approx 3.28 \times 10^{-7} \biggl( {T_{\rm e} \over 10^4 {\rm ~K} } \biggr)^{-1.35} \biggl( {\nu \over {\rm GHz} } \biggr)^{-2.1} \biggl( { EM \over {\rm pc~cm}^{-6} } \biggr)\rlap{\quad \href{FreeFreeEmission.html#TauFF}{\rm {(4B6)}}}$$
The ionization
rate $N_{\rm Ly}$ of Lyman continuum photons produced per second
required
to maintain an HII region is
$$\biggl( { N_{\rm Ly} \over {\rm s}^{-1} } \biggr) \approx 6.3 \times 10^{52 } \biggl( { T_{\rm e} \over 10^4 {\rm ~K} } \biggr)^{-0.45} \biggl( { \nu \over {\rm GHz } } \biggr)^{0.1} \biggl( { L_\nu \over 10^{20} {\rm ~W~Hz}^{-1} } \biggr)\rlap{\quad \href{FreeFreeEmission.html#LyAlphaRate}{\rm {(4B7)}}}$$
where $L_\nu = 4 \pi D^2 S_\nu$ is
the free-free luminosity at any frequency $\nu$ high enough that
$\tau_\nu \ll 1$.
The magnetic
force on a moving charge is
$$\vec{F} = { e (\vec{v} \times
\vec{B}) \over c}\rlap{\quad
\href{Magnetobremsstrahlung.html#MagneticForce}{\rm {(5A1)}}}$$
The nonrelativistic electron gyro
frequency in MHz is
$$\biggl({\nu_{\rm G} \over {\rm MHz}}\biggr) = 2.8 \biggl( { B \over
{\rm Gauss}
}\biggr)\rlap{\quad
\href{Magnetobremsstrahlung.html#ElectronGyro}{\rm {(5A3)}}}$$

$$ x = \gamma (x' + vt') \qquad y = y'
\qquad z = z' \qquad t =
\gamma (t' + \beta x' / c)\rlap{\quad
\href{SynchrotronPower.html#Lorentz}{\rm {(5B1)}}} $$
$$ x' = \gamma (x - vt) \qquad y' = y
\qquad z' = z \qquad t' = \gamma (t - \beta x / c)\rlap{\quad
\href{SynchrotronPower.html#LorentzPrime}{\rm {(5B2)}}} $$
where
$$\beta \equiv v/c\rlap{\quad
\href{SynchrotronPower.html#Beta}{\rm {(5B3)}}}$$
and
$$\gamma
\equiv (1 - \beta^2)^{-1/2}\rlap{\quad
\href{SynchrotronPower.html#Gamma}{\rm {(5B4)}}}$$
If $(\Delta x', \Delta y', \Delta z',
\Delta t')$ and $(\Delta x,
\Delta y,
\Delta z, \Delta t)$ are the coordinate differences between two
events, the differential form of the (linear) Lorentz transform is:
$$\Delta x = \gamma(\Delta x' + v
\Delta t') \qquad \Delta y =
\Delta y' \qquad \Delta z = \Delta z' \qquad \Delta t = \gamma (\Delta
t' + \beta \Delta x' / c)\rlap{\quad
\href{SynchrotronPower.html#DiffLT}{\rm {(5B5)}}} $$
$$\Delta x' = \gamma(\Delta x - v \Delta
t) \qquad \Delta y' = \Delta y \qquad \Delta z' = \Delta z \qquad
\Delta t' = \gamma (\Delta t - \beta \Delta x / c)\rlap{\quad
\href{SynchrotronPower.html#DiffLTPrime}{\rm {(5B6)}}} $$
The Thomson
cross
section of an electron is defined by
$$\sigma_{\rm T} \equiv {8 \pi \over 3} \biggl(
{ e^2 \over m_{\rm e} c^2 } \biggr)^2
\approx 6.65
\times 10^{
-25} {\rm ~cm}^2\rlap{\quad
\href{SynchrotronPower.html#ThomsonArea}{\rm {(5B7)}}}$$
Magnetic
energy density:
$$U_{\rm B} = {B^2 \over 8 \pi}\rlap{\quad
\href{SynchrotronPower.html#Umag}{\rm {(5B8)}}}$$
Synchrotron power of one electron:
$$P = 2 \sigma_{\rm T} \beta^2
\gamma^2 c\, U_{\rm B} \sin^2\alpha\rlap{\quad
\href{SynchrotronPower.html#Power}{\rm {(5B9)}}}$$
$$\langle P \rangle = {4 \over 3}
\sigma_{\rm T} \beta^2 \gamma^2 c U_{\rm B}\rlap{\quad
\href{SynchrotronPower.html#AveragePower}{\rm {(5B10)}}} $$
The synchrotron
spectrum of a single
electron is
$$P(\nu) = {\sqrt{3} e^3 B \sin \alpha
\over m c^2} \biggl( { \nu \over \nu_{
\rm c}} \biggr) \int_{\nu/\nu_{\rm c}}^\infty K_{5/3} (\eta) d
\eta\rlap{\quad
\href{SynchrotronSpectrum.html#Spectrum}{\rm {(5C1)}}}$$
where $K_{
5/3}$ is a modified Bessel function and the critical
frequency is
$$\nu_{\rm c} = {3 \over 2} \gamma^2 \nu_{\rm G}
\sin \alpha \approx \gamma^2 \nu_{\rm G} \,
\propto E^2 B_\bot \rlap{\quad
\href{SynchrotronSpectrum.html#CriticalFrequency}{\rm {(5C2)}}}$$

The synchrotron spectrum of a
single electron plotted in terms of
$$F(x) \equiv x \int_x^\infty K_{5/3} (\eta) d
\eta$$
where $x \equiv \nu / \nu_{\rm c}$.
The observed energy distribution of
cosmic-ray electrons in our
Galaxy is roughly a power law:
$$N(E) dE \approx K E^{-\delta} dE\rlap{\quad
\href{SynchrotronSrcs.html#CRSpectrum}{\rm {(5D1)}}}$$
where $N(E) dE$ is the number of
electrons per unit volume with energies $E$ to $E + dE$ and $\delta
\approx 5/2$.
The corresponding synchrotron emission coefficient is
$$\epsilon_\nu \propto B^{(\delta + 1)
/2} \nu^{(1 - \delta)/2}\rlap{\quad
\href{SynchrotronSrcs.html#EmissionSpectrum}{\rm {(5D2)}}}$$
The [negative sign
convention] spectral
index is
$$\alpha = {\delta - 1 \over 2}\rlap{\quad
\href{SynchrotronSrcs.html#SpectralIndex}{\rm {(5D3)}}}$$
For a given synchrotron luminosity,
the electron energy density is
$$U_{\rm e} \propto
B^{-3 /2} \rlap{\quad
\href{SynchrotronSrcs.html#ElectronU}{\rm {(5D4)}}}$$
The total energy density of both
cosmic rays and
magnetic
fields is
$$U = (1 + \eta) U_{\rm e} + U_{\rm B}\rlap{\quad
\href{SynchrotronSrcs.html#TotalU}{\rm {(5D5)}}}$$
where $\eta$ is the ion/electron
energy ratio.
At minimum
total energy, the ratio of
particle to
field energy is nearly unity (equipartition):
$${{\rm particle~energy} \over {\rm
field~energy}} = {(1 + \eta)
U_{\rm e} \over U_{\rm B}} = {4 \over 3}\rlap{\quad
\href{SynchrotronSrcs.html#MinimumE}{\rm {(5D6)}}}$$
The Eddington
Limit for luminosity is
$$\biggl( { L_{\rm E} \over L_\odot } \biggr) \approx 3.3 \times 10^4
\biggl( { M \over M_\odot} \biggr)\rlap{\quad
\href{SynchrotronSrcs.html#Eddington}{\rm {(5D7)}}}$$
The effective
temperature of a
relativistic electron emitting at frequency $\nu$ in magnetic
field $B$
is
$$\biggl( { T_{\rm e} \over {\rm K} } \biggr) \approx
1.18 \times 10^6 \biggl( { \nu \over {\rm Hz}} \biggr)^{1/2} \biggl( {
B \over
{\rm Gauss
}} \biggr)^{-1/2}\rlap{\quad
\href{SynchrotronSrcs.html#ElectronTemp}{\rm {(5D8)}}}$$
At a sufficiently low frequency
$\nu$,
$$S_{\rm \nu} \propto \nu^{-5/2}\rlap{\quad
\href{SynchrotronSrcs.html#SSASlope}{\rm {(5D9)}}}$$

$$\biggl( { B \over {\rm Gauss}}
\biggr) \approx 1.4 \times
10^{12} \biggl( {\nu \over {\rm Hz}} \biggr) \biggl( { T_{\rm b} \over
{\rm K} } \biggr)^{-2}\rlap{\quad
\href{SynchrotronSrcs.html#SSABfield}{\rm {(5D10)}}}$$
Nonrelativistic Thomson-scattering
power:
$$P = \sigma_{\rm T} c U_{\rm rad}\rlap{\quad
\href{InverseCompton.html#PScattered}{\rm {(5E1)}}}$$
The relativistic
Doppler equation is
$$\nu' = \nu [\gamma(1 + \beta \cos \theta)]\rlap{\quad
\href{InverseCompton.html#Doppler}{\rm {(5E2)}}}$$
The relativistic inverse-Compton
power (net) emitted is:
$$P_{\rm IC} = {4 \over 3}
\sigma_{\rm T} c \beta^2 \gamma^2 U_{\rm rad}\rlap{\quad
\href{InverseCompton.html#ICPower}{\rm {(5E3)}}}$$
IC/synchrotron
power ratio:
$${P_{\rm IC} \over P_{\rm syn} } = { U_{\rm rad} \over U_{\rm
B}}\rlap{\quad
\href{InverseCompton.html#PowerRatio}{\rm {(5E4)}}}$$
The average frequency $\langle \nu
\rangle$
of upscattered photons having initial frequency $\nu_0$ is
$${\langle \nu \rangle \over \nu_0} = {4\over
3} \gamma^2\rlap{\quad
\href{InverseCompton.html#ICFrequency}{\rm {(5E5)}}}$$
Maximum rest-frame brightness temperature of an incoherent synchrotron
source:
$$T_{\rm max} \sim 10^{12}{\rm ~K}\rlap{\quad
\href{InverseCompton.html#Tmax}{\rm {(5E6)}}}$$

The
apparent
transverse
velocity of a moving
source component is
$$\beta_\bot{\rm (apparent)} = {\beta \sin \theta \over 1 - \beta
\cos\theta}\rlap{\quad
\href{ExtraGalactic.html#ApparentBeta}{\rm {(5F1)}}}$$
The transverse ($\theta= \pi /2$)
Doppler
shift is
$${\nu \over \nu'} = \gamma^{-1}\rlap{\quad
\href{ExtraGalactic.html#TransverseDoppler}{\rm {(5F5)}}}$$
Doppler
boosting for Doppler
factor
$\delta \equiv \nu / \nu'$:
$$\delta^{2 + \alpha} < {S \over S_0} <
\delta^{3 + \alpha}\rlap{\quad
\href{ExtraGalactic.html#Boosting}{\rm {(5F6)}}}$$
Thermal and nonthermal luminosities of
star-forming galaxies:
$$\biggl({ L_{\rm T} \over {\rm
W~Hz}^{-1} } \biggr) \approx 5.5 \times 10^{20} \biggl( {\nu \over {\rm
GHz}} \biggr)^{-0.1} \biggl[ {SFR(M > 5 M_\odot) \over M_\odot {\rm
~yr}^{-1} } \biggr]\rlap{\quad
\href{ExtraGalactic.html#LThermal}{\rm {(5F7)}}}$$
$$\biggl({ L_{\rm NT} \over {\rm
W~Hz}^{-1} } \biggr) \approx 5.3 \times 10^{21} \biggl( {\nu \over {\rm
GHz}} \biggr)^{-0.8} \biggl[ {SFR(M > 5 M_\odot) \over M_\odot {\rm
~yr}^{-1} } \biggr]\rlap{\quad
\href{ExtraGalactic.html#LNonthermal}{\rm {(5F8)}}}$$
The redshift
$z$ of a source is defined by
$$(1 + z) \equiv {\lambda_{\rm observed} \over \lambda_{\rm
emitted}}\rlap{\quad
\href{ExtraGalactic.html#Redshift}{\rm {(5F9)}}}$$
