In short

Thermal radiation is electromagnetic waves emitted by every object above absolute zero. Unlike conduction and convection, it needs no medium — sunlight reaches you across ninety-three million miles of vacuum by exactly this mechanism.

Three laws govern it, and together they let you predict the glow of anything hot from its temperature alone.

  • Stefan-Boltzmann law — the total power radiated per unit surface area scales with the fourth power of temperature:
P = \sigma \varepsilon A T^{4},

with \sigma = 5.67\times 10^{-8}\,\text{W m}^{-2}\text{K}^{-4} and \varepsilon (the emissivity) between 0 and 1. The T^4 dependence is ferocious — double the temperature and you multiply radiated power by sixteen.

  • Wien's displacement law — the wavelength at which a body radiates most strongly is inversely proportional to its temperature:
\lambda_{\max} T = b = 2.898\times 10^{-3}\,\text{m\,K}.

A diya flame at 1800 K peaks in the near infrared; the Sun at 5778 K peaks in green; a human body at 310 K peaks at 9.3 microns in the thermal infrared, which is what thermal cameras see.

  • Kirchhoff's law — at a given wavelength and temperature, a surface's emissivity equals its absorptivity: \varepsilon_\lambda = \alpha_\lambda. Good absorbers are good emitters; poor absorbers (mirrors, polished metal) are poor emitters. This is why solar thermal collectors are painted black and ISRO coats satellite radiators with white ceramic.

A black body is the idealisation \varepsilon = \alpha = 1: a surface that absorbs every photon that hits it and re-emits a spectrum (the Planck spectrum) that depends on temperature alone, not on what the body is made of.

Everyday consequences sit everywhere. The cooling of a kulhad of chai has a radiation component that becomes dominant at high temperature. Rooftop solar panels in Jaipur harvest \approx 5 kWh/m² per day because the Sun is a 5778 K black body dumping \approx 1361 W/m² on the top of the atmosphere. The Earth's average temperature of 288 K is set by the radiation balance between solar input and T^4 emission back to space; take that balance seriously and you have just derived the greenhouse effect. Mangalyaan's gold-foil multilayer insulation was designed from \varepsilon_{\lambda} engineering.

Walk past a blacksmith's forge in Moradabad late at night. The iron bar in the fire is dark. Pump the bellows a few times and the bar turns a dull red. Pump more and it brightens to orange, then yellow, then a fierce white that hurts to look at. The blacksmith has not added any colour — they have only added energy. The iron is sending you photons of different wavelengths, and as it gets hotter it sends both more of them and shifts the mix toward shorter wavelengths. The sky is doing the same thing: the Sun is radiating white because its surface is at 5778 K, the Earth is radiating invisible thermal infrared because it is at 288 K, you are radiating invisible thermal infrared at 310 K, and even a block of ice at 270 K is sending out a faint infrared glow that a thermal camera can see in the dark.

This is thermal radiation, the third of the three heat transfer mechanisms. Conduction carries heat through a solid by molecular jostling. Convection carries it through a fluid by bulk flow. Radiation carries it by electromagnetic waves, and crucially, it needs no medium at all — it is how the Sun reaches you through a hundred and fifty million kilometres of vacuum. Every object above absolute zero radiates. The only question is how much and at what wavelength.

This article builds the three laws that answer those questions — the Stefan-Boltzmann T^4 law, Wien's \lambda_\max T = b law, and Kirchhoff's law relating emission to absorption. You should have read temperature and thermometers so that the T in every formula is firmly an absolute temperature in kelvin. Familiarity with electromagnetic waves is useful but not essential — all you need is that visible light, infrared, and ultraviolet are the same kind of wave, differing only in wavelength.

Every object glows — the idea of thermal radiation

Pick any object in the room. A teacup, your phone, a brick, a glacier. The atoms and molecules inside it are jiggling; if they were not, the object would be at absolute zero, which nothing real ever reaches. Jiggling atoms carry charge (electrons and nuclei) accelerating back and forth. An accelerating charge radiates electromagnetic waves — that is Maxwell's equations at work. So every object, simply by being above 0 K, is emitting electromagnetic waves from its surface.

The wavelengths this radiation contains depend on how hard the atoms are jiggling, which is to say, on temperature. A very cold object (a block of dry ice at 195 K) radiates mostly at wavelengths around 15 microns — deep infrared, invisible. A warm object (you, at 310 K) radiates at roughly 9.3 microns — near-IR, still invisible. A dull red iron bar at 800 K is now radiating with a bit of its spectrum in the visible; most of it is still infrared, but the red tail of the distribution leaks into what your eyes can see. A filament lamp at 2800 K is throwing off visible light plus a lot of waste infrared (which is why incandescent bulbs are terrible fridges). The Sun's surface at 5778 K peaks near 500 nm, smack in the middle of the visible band — which is not a coincidence: your eyes evolved sensitive to precisely the wavelengths that the Sun emits most of.

The electromagnetic spectrum with thermal-radiation ranges marked A horizontal wavelength axis from 100 nm (UV) to 100 micrometres (far IR) showing where a room-temperature human, a 1500 K iron, the Sun, and a 10000 K star each peak in emission. wavelength (micrometres, log scale) 0.1 1 10 100 1000 UV visible thermal IR far IR Sun 5778 K → 500 nm 10000 K star → 290 nm iron 1500 K → 1.93 μm human 310 K → 9.3 μm ice 270 K → 10.7 μm where does a body at temperature T peak?
The wavelength at which each body radiates most strongly, marked on the electromagnetic spectrum. The Sun lands in the visible band by coincidence of its surface temperature; everything at room temperature radiates in the thermal infrared and is invisible to the eye but bright to a thermal camera.

Three quantitative laws describe this picture. The first, Wien's displacement law, says where on the wavelength axis the peak sits. The second, Stefan-Boltzmann, says how much total power is radiated. The third, Kirchhoff's law, says how emission compares to absorption for a given surface. You can derive all three (or at least motivate them) from the idea of a black body and the equilibrium between a surface and the radiation around it — that is the work of the rest of this article.

The black body — the reference standard

The three laws each involve the notion of a black body: an idealised surface that absorbs every photon of every wavelength that hits it, reflecting and transmitting nothing. Call its absorptivity \alpha = 1. A black body is the cleanest possible emitter as well: because nothing is being reflected back and interfering with its own thermal emission, the spectrum it radiates is purely a function of its temperature, not of what it is made of. This is the key insight — the black body's spectrum is universal.

Real surfaces are not perfectly black. Polished aluminium absorbs only a few percent of the light that hits it and reflects the rest; lampblack soot absorbs about 99%; the inner wall of a hollow cavity with a small hole is almost indistinguishable from a perfect black body because any light that enters the hole rattles around and gets absorbed before it finds its way back out. The small hole in an opaque cavity — an isothermal cavity — is in fact how physicists in the 19th century built black bodies in the lab. Light going in: absorbed. Light coming out of the hole: the thermal radiation of the cavity walls, unpolluted by reflections. The spectrum of that light is what Planck worked out in 1900, and we will use his result below without deriving it (the derivation is quantum mechanics; it belongs in a separate article).

Real surfaces are described by an emissivity \varepsilon between 0 and 1, defined so that the power they emit at temperature T is

P = \varepsilon\, P_\text{black body}.

Some typical values: fresh snow \varepsilon \approx 0.8–0.9 (surprisingly close to black in the IR), skin \varepsilon \approx 0.98 (almost perfectly black in the IR — this is why you show up clearly on a thermal camera regardless of skin colour, which only affects visible light), polished aluminium \varepsilon \approx 0.05, oxidised copper \varepsilon \approx 0.6, a diya's clay pot \varepsilon \approx 0.9. The numbers are wavelength-dependent in general — a surface can be black to visible light and shiny to IR (snow is one example: white to your eyes, nearly black to a thermal camera). When you see \varepsilon without a subscript, it usually means the "total" emissivity averaged over the spectrum the body is actually emitting at that temperature.

Assumption that runs through this article: unless stated otherwise, we talk about surfaces where \varepsilon is roughly constant across the relevant wavelengths. Real surfaces are often more interesting — the "selective surface" coatings on solar hot-water panels are engineered to have high \varepsilon at visible wavelengths (to absorb sunlight) and low \varepsilon at IR wavelengths (to suppress their own thermal losses). We flag these cases when they come up.

The Planck spectrum — what a black body actually radiates

Before you can derive Stefan-Boltzmann or Wien, you need to know what a black body radiates at each wavelength. That is the Planck spectrum, the spectral radiance of a black body at temperature T:

u(\lambda, T) = \frac{2\pi h c^2}{\lambda^5}\,\frac{1}{e^{hc/(\lambda k_B T)} - 1},

where h = 6.626\times 10^{-34} J·s is Planck's constant, c = 3\times 10^{8} m/s, k_B = 1.38\times 10^{-23} J/K is Boltzmann's constant, and u(\lambda,T)\,d\lambda is the power radiated per unit surface area of the body in the wavelength interval \lambda to \lambda + d\lambda. Deriving this formula from first principles requires quantum mechanics (Planck had to assume that an oscillator could only take discrete energies n h\nu to make the integral finite — that assumption was the beginning of quantum physics). We will not re-derive it here; for this article, take it as the experimentally verified spectrum and use it to derive Wien and Stefan-Boltzmann.

Planck spectra at four temperatures (labelled in kelvin, wavelength in micrometres, radiance in arbitrary units). Each curve's peak shifts left as $T$ rises — that is Wien's displacement law visible to the eye. The area under each curve is the total radiated power, and it is rising much faster than $T$ — that is Stefan-Boltzmann.

Two features of this curve are what the two laws capture:

  1. It has a peak. The peak wavelength \lambda_\max depends on T.
  2. The area under it is the total radiated power. The total rises steeply with T.

Wien says where the peak is. Stefan-Boltzmann says what the area is. Both come out of the Planck spectrum by calculus.

Wien's displacement law — from the peak of the Planck curve

Claim: at temperature T the wavelength at which a black body radiates most strongly is

\lambda_\max T = b, \quad b = 2.898\times 10^{-3}\,\text{m\,K}. \tag{1}

Triple the temperature, the peak moves to one-third the wavelength.

Derivation. You find the peak of u(\lambda,T) by \frac{\partial u}{\partial \lambda} = 0. Let x = hc/(\lambda k_B T) so that the \lambda-dependence of the Planck expression becomes tidy.

Step 1. Write the spectrum in terms of x. Since \lambda = hc/(x k_B T), the factor 1/\lambda^5 becomes (x k_B T/(hc))^5, and the spectrum becomes

u \propto \frac{x^5}{e^x - 1}.

Why: pulling the T-dependence and the constants out of the way reduces the problem to finding the maximum of a single function of a dimensionless variable x. The answer for \lambda_\max will follow by untwisting the substitution.

Step 2. Differentiate f(x) = x^5/(e^x - 1) and set the derivative to zero.

\frac{df}{dx} = \frac{5 x^4 (e^x - 1) - x^5 e^x}{(e^x - 1)^2} = 0.

Set the numerator to zero and divide by x^4:

5(e^x - 1) - x e^x = 0 \quad \Rightarrow \quad 5 - x = 5 e^{-x}. \tag{2}

Why: the quotient rule plus the fact that e^x - 1 > 0 for x > 0 means only the numerator needs to vanish. The x^4 factor gets cancelled because x = 0 is a minimum (the spectrum vanishes at very short wavelengths), not a maximum.

Step 3. Solve the transcendental equation 5 - x = 5 e^{-x} numerically. Starting from x = 5 and iterating, you get x \approx 4.965.

Why: this equation has no closed-form solution, but one iteration of Newton's method converges quickly: x_{n+1} = 5 - 5 e^{-x_n}, with x_0 = 5 giving x_1 = 4.966, x_2 = 4.965. That is as far as you need to go.

Step 4. Untwist the substitution. x = hc/(\lambda_\max k_B T) = 4.965, so

\lambda_\max T = \frac{hc}{4.965\, k_B}.

Plug in h, c, k_B:

\lambda_\max T = \frac{(6.626\times 10^{-34})(3.0\times 10^{8})}{4.965 \times 1.38\times 10^{-23}} = 2.898\times 10^{-3}\,\text{m\,K}.

Why: the constants gather into a single universal number b — the Wien displacement constant. The equation \lambda_\max T = b is a statement about a fundamental combination of h, c, k_B, not about any particular body.

Wien's law is a stunningly useful diagnostic. Point a spectrometer at a distant star, measure its peak wavelength, and you have its surface temperature without ever touching it. Bring the same reasoning indoors: a diya flame glowing dull red must be at roughly 2.898\times 10^{-3}/(700\times 10^{-9}) \approx 4140 K if 700 nm is really where its peak lies — but careful observation suggests the flame peak is actually in the near-IR around 1600 nm, which gives T \approx 1810 K, a far more realistic diya temperature. The red your eye sees is only the short-wavelength tail of a much broader IR emission.

Interactive: drag the temperature, watch the peak shift

Interactive: peak wavelength of a black body as temperature varies A plot of peak wavelength lambda-max versus temperature. The curve is lambda-max = 2898/T. A draggable dot lets you slide along the temperature axis; readouts show T and the corresponding peak wavelength. temperature T (K) peak wavelength λ_max (μm) 0 6 15 1000 3000 5000 drag the red point along T
Drag the red point along the temperature axis to change $T$. The red curve is $\lambda_\max = b/T$ (Wien's law); the vertical dashed line shows the current temperature. At $T = 300$ K (room temperature) the peak wavelength is about 9.7 μm, deep in the thermal infrared. At $T = 5778$ K (the Sun) the peak is 0.50 μm, in the green of the visible band. The curve is a rectangular hyperbola — double the temperature, halve the peak wavelength.

The Stefan-Boltzmann law — total radiated power

Claim: the total power per unit surface area radiated by a black body at temperature T is

\frac{P}{A} = \sigma T^4, \quad \sigma = 5.67\times 10^{-8}\,\text{W m}^{-2}\text{K}^{-4}. \tag{3}

For a real surface with emissivity \varepsilon, multiply by \varepsilon: P/A = \varepsilon \sigma T^4.

Derivation. The total radiated power per unit area is the integral of the Planck spectrum over all wavelengths:

\frac{P}{A} = \int_0^\infty u(\lambda, T)\, d\lambda = \int_0^\infty \frac{2\pi h c^2}{\lambda^5}\,\frac{1}{e^{hc/(\lambda k_B T)} - 1}\,d\lambda.

Step 1. Substitute x = hc/(\lambda k_B T), so \lambda = hc/(x k_B T) and d\lambda = -hc/(x^2 k_B T)\,dx. Reversing the limits (as \lambda goes 0\to\infty, x goes \infty \to 0) absorbs the minus sign:

\frac{P}{A} = \frac{2\pi h c^2}{(hc/(k_B T))^4} \int_0^\infty \frac{x^3}{e^x - 1}\,dx \cdot \frac{1}{hc}\cdot\frac{1}{k_B T}.

Tidying the powers of h, c, k_B, T:

\frac{P}{A} = \frac{2\pi k_B^4 T^4}{h^3 c^2} \int_0^\infty \frac{x^3}{e^x - 1}\,dx. \tag{4}

Why: this substitution is the standard move — it separates the T-dependence cleanly, leaving a dimensionless integral that is a pure number. The T^4 is already visible in front of the integral; that is the origin of the fourth-power law.

Step 2. Evaluate the dimensionless integral. It is a standard result in mathematical physics:

\int_0^\infty \frac{x^3}{e^x - 1}\,dx = \Gamma(4)\,\zeta(4) = 6 \cdot \frac{\pi^4}{90} = \frac{\pi^4}{15}.

Why: expand 1/(e^x - 1) = \sum_{n=1}^\infty e^{-nx} (a geometric series, valid for x > 0) and integrate term by term to get \sum_{n=1}^\infty 6/n^4 = 6\,\zeta(4) = \pi^4/15. Knowing \zeta(4) = \pi^4/90 from the theory of the Riemann zeta function closes the calculation. If this detail is new, read it as "the integral evaluates to about 6.49" and move on; the rest of the derivation does not depend on knowing why.

Step 3. Put it together:

\frac{P}{A} = \frac{2\pi k_B^4}{h^3 c^2}\cdot \frac{\pi^4}{15} \cdot T^4 = \frac{2\pi^5 k_B^4}{15\, h^3 c^2}\, T^4 = \sigma T^4. \tag{5}

With numerical values plugged in:

\sigma = \frac{2\pi^5 (1.381\times 10^{-23})^4}{15\,(6.626\times 10^{-34})^3 (3\times 10^{8})^2} = 5.67\times 10^{-8}\,\text{W m}^{-2}\text{K}^{-4}.

Why: the Stefan-Boltzmann constant \sigma is a combination of fundamental constants alone. The T^4 is the key physics — it makes the power rise with extraordinary steepness. Go from 300 K to 600 K, the power rises by a factor of 2^4 = 16. Go from 300 K to 6000 K (as the Sun does), it rises by 20^4 = 160{,}000.

For a real surface, replace \sigma by \varepsilon\sigma. For a body at temperature T sitting in surroundings at temperature T_s, the net rate at which it loses energy to radiation is

\frac{P_\text{net}}{A} = \varepsilon\sigma(T^4 - T_s^4), \tag{6}

because the body emits \varepsilon\sigma T^4 and absorbs \varepsilon\sigma T_s^4 from the surroundings (by Kirchhoff's law, its absorptivity equals its emissivity — we prove this in the next section). This is the form that matters for heat-loss calculations: a cup of chai losing heat to a room, a satellite losing heat to the 2.7 K cosmic background, the Earth losing heat to space.

Assumption check: equation (6) assumes the surroundings are themselves approximately a black body at temperature T_s (the walls of a room, the sky as a whole, etc.). If the surroundings have a different emissivity, you need a more general "form factor" analysis, which belongs in an engineering heat-transfer text.

Kirchhoff's law — good absorbers are good emitters

Claim: at any given wavelength and temperature, a body's emissivity equals its absorptivity:

\varepsilon_\lambda(T) = \alpha_\lambda(T). \tag{7}

Derivation. Place any object inside an isothermal cavity at temperature T. The cavity is full of black-body radiation at temperature T with spectrum u(\lambda, T). In thermal equilibrium the object must be at the same temperature T — any other temperature would imply a net energy flow that would change its temperature, contradicting equilibrium.

Thermal equilibrium requires detailed balance at every wavelength. The power the object absorbs from the radiation in wavelength interval d\lambda is

dP_\text{abs} = \alpha_\lambda(T)\, u(\lambda, T)\, A\, d\lambda.

The power it emits in the same wavelength interval is

dP_\text{em} = \varepsilon_\lambda(T)\, u(\lambda, T)\, A\, d\lambda,

because \varepsilon_\lambda u(\lambda, T) is by definition the body's emission compared to a black body's.

Why: a black body would emit u(\lambda, T)\, A\, d\lambda in that wavelength interval. A real body emits \varepsilon_\lambda times that. The absorptivity \alpha_\lambda is defined as the fraction of incident radiation the body absorbs at wavelength \lambda.

In equilibrium, the two must be equal (otherwise energy at wavelength \lambda would accumulate or deplete, contradicting the steady state):

\alpha_\lambda(T)\, u(\lambda, T) = \varepsilon_\lambda(T)\, u(\lambda, T) \quad \Rightarrow \quad \alpha_\lambda(T) = \varepsilon_\lambda(T).

Since this must hold for every wavelength independently (radiation at different wavelengths does not interconvert in equilibrium), it is a point-wise equality, not a spectrum-averaged one.

Why the detail balance? If the absorption rate at some \lambda exceeded the emission rate, energy at \lambda would decrease in the cavity until that wavelength's radiation dropped and equilibrium was restored — but then the cavity radiation would no longer match the universal u(\lambda, T), which contradicts the known universality of black-body radiation. So emission and absorption have to match independently at every wavelength.

Kirchhoff's law has three immediate practical consequences.

  1. A good absorber is a good emitter. A black surface (high \alpha) at temperature T radiates more than a shiny surface at the same temperature. That is why solar collectors are painted black — they absorb more sunlight and, as a bonus, emit their own infrared well (but this IR loss is a problem that selective surfaces solve).

  2. Polished metal radiates very little. An aluminised surface at 300 K emits at maybe 5% of the black-body rate. That is why Dewar flasks (thermos bottles) have silvered inner walls — radiation loss from the hot liquid is cut by a factor of 20 compared to a black bottle.

  3. "Thermally transparent" means cannot radiate. A window pane that transmits visible light is not radiating visible light. But glass is nearly black in the thermal IR (\varepsilon \approx 0.95 at 10 μm) and radiates like a black body at window temperature — which is why your thermal camera sees you through a glass pane only partially. It sees the pane's IR emission superimposed on the room's IR reflections.

Worked examples

Example 1: Power radiated by a rooftop solar panel and by the Sun

A flat-plate solar thermal collector on a Jaipur rooftop is a 1\,\text{m}^2 black-coated copper surface with emissivity \varepsilon = 0.95. When in steady-state operation, it reaches 80 °C (= 353 K) on a clear afternoon when the sky's effective radiating temperature is 260 K. Find the power it radiates back to the sky, and compare to the power it receives from the Sun.

Energy balance of a rooftop solar collector Schematic of a 1 m² flat-plate collector receiving 950 W from the Sun, radiating about 660 W back as IR, and keeping roughly 290 W as useful heat. collector at 353 K, 1 m², ε = 0.95 Sun in: ≈ 950 W IR out: ≈ 660 W useful ≈ 290 W
The collector's three energy flows. Solar in is 950 W, IR radiation out is 660 W, and the rest is what the water-carrying pipes underneath collect as useful heat.

Step 1. Set up the equation. The collector is losing heat to the sky by radiation, so use the net Stefan-Boltzmann form

P_\text{rad} = \varepsilon \sigma A (T^4 - T_s^4).

Why: the collector emits \varepsilon\sigma A T^4 and absorbs \varepsilon\sigma A T_s^4 from the cold sky (Kirchhoff's law). The difference is the net outflow to the sky by radiation.

Step 2. Plug in numbers. \varepsilon = 0.95, \sigma = 5.67\times 10^{-8} W m⁻² K⁻⁴, A = 1\,\text{m}^2, T = 353 K, T_s = 260 K.

T^4 = 353^4 = 1.553\times 10^{10}\,\text{K}^4, \qquad T_s^4 = 260^4 = 4.570\times 10^{9}\,\text{K}^4.
P_\text{rad} = 0.95 \times 5.67\times 10^{-8} \times 1 \times (1.553\times 10^{10} - 4.570\times 10^{9})
P_\text{rad} = 0.95 \times 5.67\times 10^{-8} \times 1.096\times 10^{10} = 590\,\text{W}.

Why: note the ferocity of the fourth-power law. The collector is only about 93 K hotter than the sky, but it is dumping nearly 600 W per square metre into the sky. Even a modest temperature difference compounds hard.

Step 3. Compare with solar input. Jaipur's peak solar irradiance on a south-facing tilted surface in March is about 950\,\text{W/m}^2 (global normal). The collector absorbs \alpha \times 950 W; for a well-designed black selective coating, \alpha \approx 0.95 in the visible too, giving P_\text{in} \approx 900\,\text{W}.

P_\text{useful} = P_\text{in} - P_\text{rad} - P_\text{convection} - P_\text{conduction}.

With convection and conduction losses of roughly 10 W total (a good selective surface plus a glass cover plus insulation at the back), the useful heat extracted is

P_\text{useful} \approx 900 - 590 - 10 \approx 300\,\text{W}.

Why: the collector's radiation loss is the dominant loss. A selective-surface coating reduces ε in the IR to around 0.1 while keeping α in the visible near 0.95, and that drops P_\text{rad} by a factor of about 10 — which is why every serious solar thermal collector uses one.

Step 4. Per-day energy harvest. Over 5 peak-equivalent hours of sun per day in Jaipur,

E_\text{day} = 300\,\text{W} \times 5\,\text{h} = 1.5\,\text{kWh per day per square metre}.

Result: A 1 m² flat-plate collector loses about 590 W by radiation, keeps roughly 300 W of the 900 W arriving from the Sun, and delivers about 1.5 kWh of useful heat per day. A domestic 100-litre solar water heater (2 m² panel) will warm its water by \Delta T \approx 3000\text{ Wh}/(100\text{ kg} \cdot 4180\text{ J/kg/K}) \approx 25 K per day — which is exactly what Jaipur residents see on their bathroom geysers.

What this shows: the T^4 dependence means radiation losses dominate any surface operating well above ambient. Selective surfaces (engineered to have high \alpha at solar wavelengths and low \varepsilon in the thermal IR) are the engineering solution. The whole economics of solar thermal in India depend on this.

Example 2: Surface temperature of the Sun from a peak-wavelength measurement

The Sun's peak spectral radiance sits at a wavelength of \lambda_\max = 501 nm. Using Wien's displacement law, estimate the temperature of the Sun's surface, and then use Stefan-Boltzmann to estimate the total power output of the Sun. The Sun's radius is R_\odot = 6.96\times 10^{8} m. Assume the Sun radiates as a black body (\varepsilon \approx 1).

Black-body spectrum of the Sun with peak marked at 501 nm A sketched Planck curve from 100 nm to 2500 nm with a peak at 501 nm and a vertical dashed line labeled lambda-max. wavelength λ (nm) 100 500 1000 2500 λ_max = 501 nm
The observed solar spectrum with its peak at 501 nm. Plugging into Wien's law gives a surface temperature of about 5780 K.

Step 1. Apply Wien's law.

T = \frac{b}{\lambda_\max} = \frac{2.898\times 10^{-3}}{501\times 10^{-9}} = 5786\,\text{K}.

Why: Wien's law lets you read off a body's temperature from its spectrum. The Sun's surface is hot enough to radiate most of its power in visible wavelengths — which is why human vision is tuned to this band.

Step 2. Apply Stefan-Boltzmann.

\frac{P}{A} = \sigma T^4 = 5.67\times 10^{-8} \times (5786)^4 = 5.67\times 10^{-8} \times 1.12\times 10^{15} = 6.35\times 10^{7}\,\text{W/m}^{2}.

Why: this is the solar surface's radiant flux — about 63 megawatts per square metre. Compare to 1000 W/m² at the Earth's surface on a sunny day; the extra factor of 60{,}000 is essentially the Sun's T^4 relative to Earth's.

Step 3. Multiply by the solar surface area to get total luminosity.

A_\odot = 4\pi R_\odot^2 = 4\pi (6.96\times 10^{8})^2 = 6.09\times 10^{18}\,\text{m}^2.
L_\odot = 6.35\times 10^{7}\times 6.09\times 10^{18} = 3.87\times 10^{26}\,\text{W}.

Step 4. Sanity-check against the solar irradiance at Earth. The Earth's mean orbital radius is r = 1.496\times 10^{11} m. At that distance, the flux is

S = \frac{L_\odot}{4\pi r^2} = \frac{3.87\times 10^{26}}{4\pi (1.496\times 10^{11})^2} = 1375\,\text{W/m}^{2}.

Why: the spherical geometry spreads the Sun's output over a sphere of radius one AU. The measured "solar constant" at the top of Earth's atmosphere is 1361 W/m², so our prediction is within 1% — the T^4 law and the Wien-derived temperature are both accurate to the measurement precision of this problem.

Result: the Sun's surface temperature is 5786 K, its luminosity is 3.87\times 10^{26} W, and the solar constant predicted at Earth is 1375 W/m² — all from one peak-wavelength measurement plus two laws.

What this shows: Wien plus Stefan-Boltzmann together let you reconstruct the entire energy output of a distant star from a single spectral measurement. Every stellar mass estimate, every exoplanet equilibrium temperature, every ISRO thermal-control calculation uses exactly this pair of equations.

Example 3: Earth's surface temperature from radiation balance

Estimate the equilibrium surface temperature of the Earth assuming the Earth radiates as a black body and that 30% of incoming solar radiation is reflected by clouds, ice, and bright surfaces (the "albedo" A_\text{albedo} = 0.30). The solar constant is S = 1361\,\text{W/m}^2.

Energy balance for Earth Schematic showing sunlight falling on Earth's cross-sectional area, 30% reflected, and Earth re-radiating from its full surface area at temperature T. Earth, T, area 4πR² S(1−A) πR² σT⁴ × 4πR²
Solar radiation intercepts a disk of area $\pi R^2$; the Earth re-radiates from its full surface $4\pi R^2$. Setting absorbed equal to emitted in equilibrium gives the Earth's radiative temperature.

Step 1. Write the absorbed power. The Earth's cross-sectional area to the Sun (a disk of radius R) intercepts flux S, of which a fraction 1 - A_\text{albedo} is absorbed.

P_\text{abs} = S(1 - A_\text{albedo})\,\pi R^2.

Why: sunlight is effectively parallel at Earth's distance, so only the cross-section matters. Albedo is the fraction reflected back to space before absorption.

Step 2. Write the emitted power. The Earth radiates from its entire surface (4\pi R^2), not just the sunlit side, because the planet rotates and the thermal emission is roughly isotropic.

P_\text{em} = \sigma T^4 \cdot 4\pi R^2.

Why: Stefan-Boltzmann for a black body. Using \varepsilon = 1 is a common first-approximation for the Earth because the planet's thermal IR emissivity is around 0.95, close enough for a back-of-envelope calculation.

Step 3. Set P_\text{abs} = P_\text{em} and solve for T.

S(1 - A_\text{albedo})\,\pi R^2 = \sigma T^4\, 4\pi R^2
T^4 = \frac{S(1 - A_\text{albedo})}{4\sigma}
T = \left[\frac{1361 \times 0.70}{4 \times 5.67\times 10^{-8}}\right]^{1/4} = \left[4.20\times 10^{9}\right]^{1/4} = 254\,\text{K}.

Why: the geometric factor 4 is the ratio of the Earth's surface area to its cross-section. Without the albedo factor (setting A_\text{albedo}=0) you get 279 K, a common textbook result for an airless, black Earth.

Step 4. Reality check. The observed Earth surface temperature is about 288 K — 34 K warmer than this prediction. The gap is the greenhouse effect: the Earth's atmosphere (mainly water vapour, CO₂, methane) is nearly transparent to visible light but strongly absorbing in the thermal IR. It lets solar radiation in, then absorbs the outgoing IR and re-radiates half of it back downward. This forces the surface to run hotter to balance the re-radiated contribution.

Result: a bare-rock Earth with 30% albedo would sit at 254 K — far below freezing, a snowball. The real Earth at 288 K is held warm by the atmosphere's selective IR absorption.

What this shows: the radiation-balance equation P_\text{abs} = P_\text{em} is the most powerful climate-physics equation there is. It sets the temperature of every planet, every satellite, every asteroid, given only the incident flux and the emissivity structure. Climate change at its heart is a perturbation to this equation: change the atmospheric IR absorption, and T^4 responds.

Common confusions

If you came here to use the three laws, you have what you need. What follows is the machinery behind them — the Rayleigh-Jeans ultraviolet catastrophe, Wien's law at the other end of the spectrum, and the satellite thermal-control problem that exercises all three laws together.

The ultraviolet catastrophe and why the Planck spectrum works

Before Planck in 1900, the best classical attempt to derive the black-body spectrum was the Rayleigh-Jeans law. Treat the cavity radiation as a set of standing electromagnetic modes, assign each mode the classical equipartition energy k_B T (half for electric, half for magnetic), and count the modes per unit wavelength:

u_\text{RJ}(\lambda, T) = \frac{2\pi c\, k_B T}{\lambda^4}.

Why: standing modes in a cavity of side L have wavelengths \lambda_{n} = 2L/n for integer n in each of three dimensions; the number of modes per unit wavelength scales as \lambda^{-4} (think of the surface area of a sphere in n-space). Classical equipartition assigns k_B T per mode regardless of wavelength.

This formula works at long wavelengths — a T that the experimental spectrum approaches. But as \lambda \to 0, u_\text{RJ} \to \infty. Integrated over all wavelengths it gives infinite radiated power. This is the ultraviolet catastrophe, the word catastrophe being an understatement for the state of classical physics in 1900.

Planck's fix was to postulate that each mode could only hold discrete energies n\,h\nu = n\,hc/\lambda, so the average energy per mode is no longer k_B T but

\langle E\rangle = \frac{hc/\lambda}{e^{hc/(\lambda k_B T)} - 1}.

This is the Bose-Einstein occupation factor for photons — a uniquely Indian connection, because Satyendra Nath Bose's 1924 paper showed that the correct statistics for photons followed from treating them as identical indistinguishable particles. Einstein took Bose's paper to heart and extended it to massive particles, giving what we now call Bose-Einstein statistics. Every time you write the 1/(e^{hc/(\lambda k_B T)}-1) factor, you are using Bose's result.

The Planck factor reduces to k_B T at long wavelengths (small hc/\lambda, Taylor-expand the exponential) — reproducing Rayleigh-Jeans. At short wavelengths it suppresses modes exponentially, killing the catastrophe. This is the single sentence that gave birth to quantum physics.

Wien's law at short wavelengths

At the opposite limit — very short wavelengths, hc/(\lambda k_B T) \gg 1 — the Planck spectrum reduces to

u_\text{Wien}(\lambda, T) = \frac{2\pi hc^2}{\lambda^5}\, e^{-hc/(\lambda k_B T)}.

This is Wien's radiation law (historically a guess before Planck). It is excellent at short wavelengths but fails at long wavelengths (where Rayleigh-Jeans is correct). Planck's formula interpolates between the two and is right everywhere.

Satellite thermal control — the Mangalyaan problem

Mangalyaan (the Mars Orbiter Mission, launched 2013) faced a thermal-control problem that exercises every law in this article. The spacecraft receives S = 590\,\text{W/m}^2 of sunlight at Mars' orbital distance (about 1.52 AU, so S = 1361/1.52^2). Its internal electronics dissipate roughly 150 W. It must stay between 273 K and 313 K during its mission.

If the spacecraft were a simple black sphere of radius R_\text{sat}, its equilibrium temperature would be

T = \left[\frac{S(1-A) + P_\text{internal}/(\pi R_\text{sat}^2)}{4\sigma}\right]^{1/4}.

For R_\text{sat} = 0.5 m (Mangalyaan's rough size), P_\text{internal}/(\pi R_\text{sat}^2) = 191\,\text{W/m}^2, and assuming A = 0, T = [781/(4\cdot 5.67\times 10^{-8})]^{1/4} \approx 342 K — too hot.

Engineers solve this by wrapping the spacecraft in multi-layer insulation (MLI) — the gold-coloured foil you see in pictures of every spacecraft. MLI consists of alternating sheets of aluminised mylar; each sheet has emissivity \varepsilon \approx 0.03 on both sides. Twenty layers reduce heat flux by roughly a factor of 20 (each layer adds to the total radiative resistance). This blocks both solar heating and internal heat leaking outward, letting the spacecraft use small electrical heaters and radiators to hold the temperature within the required window.

Crucially, the radiator panels — where the spacecraft dumps its waste heat — are white ceramic paint: high \varepsilon in the thermal IR (so they emit well), low \alpha in the visible (so they absorb minimal sunlight). That is a selective surface tuned by Kirchhoff's law. You paint the hot panels white and they happily radiate 150 W to deep space, staying at around 300 K.

When future ISRO missions send probes further out (Shukrayaan to Venus, or a potential Jovian mission), the thermal-balance numbers change dramatically, but the machinery is the same three laws you have now derived.

Why the T^4 law holds classically even without quantum mechanics

It is worth noting that the form P = \sigma T^4 can be derived from pure thermodynamics without ever invoking the Planck spectrum, using Wien's thermodynamic argument that combines Maxwell's equations with the second law. The thermodynamic argument fixes the T^4 scaling uniquely — what it cannot do is compute the coefficient \sigma, because that requires knowing the density of electromagnetic modes, which requires quantum mechanics (or at least a specific model of the wave mechanics of cavities). So the exponent 4 is "safe" to teach as a classical fact, while the numerical value of \sigma belongs to the quantum era.

Greenhouse effect — why the real Earth is warmer

We saw that a bare-rock Earth with 30% albedo sits at 254 K, but the real surface is at 288 K. A simple one-layer model of the atmosphere gives you the 34 K gap. Assume a single atmospheric layer at temperature T_A that is transparent to visible light (so all solar radiation reaches the surface) and a black body in the thermal IR (so it absorbs all outgoing IR from the surface and re-emits half up, half down). Energy balance:

  • Atmosphere: IR absorbed from surface = IR emitted up + IR emitted down, giving \sigma T_S^4 = 2\sigma T_A^4, so T_A = T_S/2^{1/4}.
  • Surface: solar in + IR back from atmosphere = IR emitted up, giving S(1-A)/4 + \sigma T_A^4 = \sigma T_S^4.

Substituting T_A^4 = T_S^4/2:

\frac{S(1-A)}{4} + \frac{\sigma T_S^4}{2} = \sigma T_S^4 \quad \Rightarrow \quad T_S^4 = \frac{S(1-A)}{2\sigma} \quad \Rightarrow \quad T_S = 2^{1/4}\cdot 254 = 302\,\text{K}.

Closer to the observed 288 K. A more realistic atmosphere (partially transparent to IR, multiple layers, clouds, latent heat) gets you the remaining 14 K. But the key point — that IR-absorbing gases raise the surface temperature by a factor of 2^{1/4} over the bare value — is captured by the one-layer model and comes out directly from the Stefan-Boltzmann T^4 law.

Where this leads next