Sunlight on Earth – Black Nights , Blue Days

Introduction

Have you ever thought about why the sky is blue most of the day and why sunrises and sunsets usually involve orange/red colors?

The answer is that nitrogen and oxygen molecules (mostly) in the Earth’s atmosphere preferentially scatter certain components of sunlight. 

These components of sunlight are often described by energy or wavelength or frequency. 

Lower wavelength light (on the purple/blue side in the picture below) simply scatters more than the longer wavelength light (the right orange/red part)  

Picture: Visible Spectrum

Scattering Simply Explained

If you looked directly at the sun (don’t do that), during noon lets say, you would see white. 

  • White is simply the mix of all the visible colors shown above (remember that mnemonic ROYGBIV?) 
  • But if you look at the open sky away from the sun, what do you see? You will see some shade of blue. 
  • The blue component of light scatters more than the others colors so you see that color. 

Well why don’t we see purple light scattered in the sky? Because it is true that it has a shorter wavelength than blue. There are two reasons for this.

  • The intensity of the light in the purple range is weaker than the blue light
  • Our retinal photo cells more naturally see blue vs purple

Why do we see Orange/Reg at Sunrise and Sunset

From your position, sunlight from the sun at the horizon (at sunrise or sunset) has to travel the furthest distance through the atmosphere to get to your eyes

  • The distance through the atmosphere the light must go through is (roughly) 38 times more than when the sun is roughly straight above you.
  • You can often look directly at the sun as it begins its ascent/descent.
  • The shorter wavelengths have been completely scattered out as you look straight at the sun. 
  • So you see the high wavelength portion of the visible spectrum (the right side of the picture above i.e., orange and red).
  • If you look away from the sun or above the sun, you will of course still see blue. 

 

In this post, we’ll dig deeper to uncover some of the physics at play. 

  • I’ll start at the source, exploring the raw energy of the Sun and how we compute the solar constant.
  • From there, I’ll trace how Earth’s atmosphere acts as a multi-layered filter, reducing solar radiation through ozone reactions, absorption, reflection, and scattering.

While every mechanism plays its part, the primary focus of this post is Rayleigh scattering ; the fundamental phenomenon responsible for the sky’s shifting colors.

We’ll break down the basic variables in its computation, examine the solar spectrum at both the top of the atmosphere and sea level to see where attenuation strikes hardest, and finally, we’ll derive the scattering cross-section equation.

Using it alongside a few key physical relationships, we will build a practical percentage scattering chart from the ground up.

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Energy From The Sun 

In order for us to understand climate on Earth, we have to understand how much energy it’s receiving from the Sun.

Inverse Square Law

Light energy must dilute in proportion to the expanding spherical area it travels.

The astronomer Johannes Kepler first articulated this in 1604. 

Picture: Sunlight Irradiance and the Inverse Square Law

The total solar power (S for Solar power; or P for Power; or L for Luminosity) is the total radiant power (SI units = Watt = J/s) coming out of the Sun in all directions. 

We can compute the amount of solar electromagnetic power (or radiant flux) received by a surface per unit area (the irradiance) as follows:

  • I = Irradiance or flux density is the solar power received by a surface per unit area. 
  • Using the inverse square law, you take the Sun’s total output power (P), and spread it out over the surface area of an expanding imaginary sphere of radius r , (4π r²),  centered on the Sun.
  • When that energy hits Earth, you are calculating how much power is arriving per unit area.
  • Units of measure: Power per unit area (Watts / m² = W / m² ). 

i.e. , solar irradiance on a particular body in space is inversely proportional to the surface area of a sphere whose center is the Sun and whose radius is equal to the distance from that body to the Sun.

(ES1) I = S / (4πr2) ; Irradiance = Radiant Flux Density, or Intensity.

where

  • I = solar irradiance = flux density  (in Watts / m² = W / m² )
  • S = total solar power (S for Solar power; or P for Power; or L for Luminosity) = the total radiant power (SI units = Watt = J/s) coming out of the Sun in all directions. 
  • r = distance from Sun to object.
  • For Earth r =  149.6 million kilometers (about 93 million miles) = 1 Astronomical Unit = 1 au

Today we use a tool called an Electrical Substitution Radiometer to measure solar irradiance at the top of the Earth’s atmosphere (about 400 to 800 km or 250 to 500 miles above surface of Earth). 

For Earth,  Isun-earth = 1361 Watts/m2   

(ES2) Isun-earth = 1361 Watts/m2 ; Solar Constant = Solar Irradiance (flux density) at the Top of the Earth’s Atmosphere 

The Solar Constant is the average amount of solar electromagnetic radiation received per unit area at the top of Earth’s atmosphere, measured on a surface perpendicular to the Sun’s rays at a distance of one astronomical unit (distance from Sun to Earth).

So what is the value of S, the total solar power? 

  • The distance of the Earth from the Sun (astronomical unit)  is 149.6 million kilometers (about 93 million miles). 
  • So we can calculate the total power of the Sun from the Inverse Square Law
  • S = Isun-earth4πr2
  • S = (1361 W/m2)(4π)(1.496×1011 meters)2

S = 3.8275..x 1026 Watts = 383 trillion trillion Watts = 383 Septillion Watts

For our discussions I is the important number, but just be aware that S is just mind – bogglingly large.   

Average Power/m2 of Sun on Earth

Ok, we need to now average this solar constant  (Isun-earth = 1361 Watts/m2 ) to the surface area of the Earth. 

Check out my picture below as you read this section. 

Picture: Average Solar Radiation is Solar Constant/4

From the perspective of the Sun, the rays hitting the Earth are hitting a circular area with a radius equal to the Earth’s radius . 

Imagine the light is a layer of paint spread out over this 2D Earth circle of area re. 

  • The total power in this circular area, Pdisk , on average, has to cover the whole surface area of the Earth.
  • So, using the paint analogy, applying that layer of paint around the full sphere of Earth will thin it out or dilute it.
  • So Iearth , the average solar radiation at Earth will be = Pdisk /area of the Earth

Let’s do the math and see what kind of expression we can get for Iearth

We know that,  

Isun-earth = Solar Constant = 1361 W/m2

We can express the power of the Sun rays on that disk, in SI units of Watts, as  Pdisk . This can be expressed as

  • Isun-earthAdisk  = Pdisk

where Adisk  is the area of the circle with radius re (the radius of the Earth) that the light rays are hitting:

  • Adisk  =  πr2e

The Sun’s power in Pdisk must be applied across the whole surface area of the Earth.

  • Iearth =  Pdisk / Aearth

Where

  • Iearth  =  Average Solar Radiation = Top of Atmosphere Insolation = Mean Global Solar Flux
  • Aearth =  Surface area of the Earth as a sphere:  4πr2e

Substitute equations 1 and 2 and the expression for Aearth  into equation 3 to get. 

  • Iearth =  Isun-earthAdisk / Aearth =  Isun-earth πr2e /4πr2e 

This simplifies to

(ES3) Iearth =  Isun-earth / 4 = 1361/4 = 340 W/m2; Average Solar Radiation = Top of Atmosphere Insolation = Mean Global Solar Flux Density

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Solar Radiation Attenuation (Depletion, Extinction)

Of course, because of Earth’s rotation, for roughly half the time, there is no sunlight.

When there is sunlight, it hits the Earth and travels down to the surface, but,  it does not arrive with 100 percent of its original power.

Along the way, the Earth’s atmosphere filters a large portion of the total solar energy by reflection, scattering, and absorption.

Solar radiation attenuation refers to the gradual reduction in the intensity of electromagnetic radiation as it passes through a medium like the atmosphere.

In the picture below,  I show the major forms of solar radiation attenuation (reduction, removal). 

I also show for completeness that Earth absorbs some solar radiation and emits infrared radiation, which then gets absorbed and re-emitted (with a portion of it eventually escaping the atmosphere into space).

This IR absorption and re-emittance is the integral mechanism of global warming which I cover in this article (Global Warming Primer).

Picture: Solar Radiation Attenuation

 

We can describe four different types of attenuation: 

1. Upper Atmospheric Reaction with Ozone (UV Absorption)

The stratosphere effectively filters out the most dangerous components of solar radiation through dedicated photolytic destruction.

  • UV-C is 100% absorbed and destroyed as high-energy photons break apart molecular oxygen and ozone, while UV-B is 90% to 95% removed by ozone absorption.
  • The byproduct of UV-C photolysis on molecular oxygen (O2) is two free oxygen atoms (O + O), whereas the photolysis of ozone (O3) by UV-B and UV-C yields one oxygen molecule (O2) and one free oxygen atom (O).
  • This protects life on Earth from harmful radiation while creating distinct temperature layers in the upper atmosphere (i.e. , photolysis produces heat).

2. Infrared (IR) Absorption

  • Some solar radiation will be directly absorbed in the atmosphere.
  • Mid-to-far infrared wavelengths, primarily associated with thermal energy, are absorbed by greenhouse gases as sunlight travels lower into the atmosphere.
  • Molecules like water vapor (H2O), carbon dioxide (CO2), and methane (CH4) possess chemical bonds that resonate with these specific infrared frequencies.
  • Upon absorbing an infrared photon, the molecule becomes excited and temporarily stores that energy before re-emitting a new infrared photon in a random direction, which traps and circulates heat within the Earth system.

3. Reflection

  • A significant fraction of incoming solar radiation is bounced directly back out into space before it can be absorbed.
  • This is driven by Earth’s albedo (reflectivity).
  • Bright surfaces like thick cloud tops, snow, and ice reflect a massive percentage of incoming shortwave radiation away from the planet, whereas dark surfaces (like oceans or dense forests) absorb it.

4. Scattering

  • Incoming sunlight collides with gas molecules, dust, and aerosols, which deflect the photons in random directions without absorbing them.
  • This is split into Rayleigh scattering (air molecules scattering shorter blue wavelengths, giving us a blue sky)
  • and Mie scattering (larger dust/smoke particles scattering all visible wavelengths more equally, causing hazy or white skies).
  • It turns a portion of direct sunlight into diffuse, scattered light.

Rayleigh Scattering

Consider the picture below showing

  • incident sunlight hitting a particle (or molecule),
  • which scatters the light in many directions,
  • and a viewer who sees the scattered radiation at some angle θs. 

Picture: Rayleigh Scattering

  • This  “Rayleigh Scattering”  drawing displays the governing mathematical relationship: 

(SA1) I ∝ (Io)(1/λ4)(1+cos2θs) ; Governing Relationship for Rayleigh Scattering

  • It illustrates an incident photon with wavelength λ and initial intensity Io  (in W/m2)
  • striking a small air molecule (such as N2 or O2) with a diameter d much smaller than the wavelength (d <<λ/10),
  • causing the light to scatter in multiple directions.
  • The incoming ray from the sun interacts with the molecule at a scattering angle , θs , dispersing blue-directional arrows outward, while a scattered ray (I) travels downward to an observer.
  • Note that while I is commonly called “Intensity,” radiometrically speaking, it actually represents irradiance (see Appendix 1 for the radiometrically correct light “type” terminology).

Mie Scattering

The diagram below compares two main types of atmospheric light scattering side-by-side:

  • Rayleigh Scattering on the left and
  • Mie Scattering on the right. 

Picture: Rayleigh vs Mie Scattering

 

Left Side: Rayleigh Scattering

  • Rayleigh Scattering occurs when d is much less than  1/10 λ    
  • So Gas molecules such as nitrogen (N2) and oxygen (O2) fit the bill. 
  • The left picture shows a central small particle surrounded by radiation scattering outward in all directions.
  • The pattern forms a symmetric, nearly uniform 360-degree distribution, illustrating that light is scattered roughly equally backward, forward, and sideways.

Right Side: Mie Scattering

  • Mie Scattering occurs when the particle diameter is larger than one-tenth of the wavelength, often equal to or larger than the wavelength itself.
  • Examples of Mie Scatterers:  Clouds, fog, smog, air pollution, smoke, and pollen.
  • The right picture shows a scattering pattern with arrows pointing outward, but the pattern is strongly asymmetric.
  • The majority of longer, prominent arrows extend to the right (forward direction along the incident light path), while much shorter arrows extend backward and sideways, demonstrating strong forward scattering

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Solar Radiation Spectrum at Earth

The chart below plots solar irradiance (W/m2 /nm wavelength) against wavelengths ranging from 250 to 2500 nm, comparing sunlight at the top of the atmosphere to sunlight at sea level.

Picture: Solar Radiation Spectrum On Earth (Cloud Free; Top of Atmosphere and at Sea Level)

  • Ozone: In the ultraviolet range (100–400 nm), ozone (O3) and molecular oxygen heavily filter out high-energy UV-C (completely) and UV-B (roughly 90–99%),
  • creating a massive drop between top-of-atmosphere baseline and sea-level irradiance in those bands.
  • Longer-wavelength UV-A (315–400 nm) is largely unabsorbed by ozone, allowing almost all of it to penetrate down to the surface.
  • Scattering: Across the visible and near-IR spectrum (roughly 380–700 nm and the upper curve envelope), attenuation is driven by Rayleigh scattering and aerosols, which scatter short wavelengths away from a direct path to the surface.
  • Absorption: In the infrared range (750–2500 nm), a series of deep troughs and dips reveals where infrared radiation is strongly absorbed by atmospheric gases, specifically oxygen (O2), carbon dioxide (CO2), and multiple water vapor (H2O) bands.

How Much Solar Radiation Gets to the Earth?

Based on the provided clear-sky engineering model (represented by the chart above), approximately 70% of incoming solar radiation reaches the Earth’s surface at sea level (1000 W/m2 out of the 1365  W/m2  top-of-atmosphere baseline). 

But in reality only about 48% of incoming solar energy actually reaches the surface globally.

This discrepancy occurs because the chart above depicts an idealized, cloud-free local maximum under standardized clear-sky conditions rather than a true 24/7 global planetary average.

  • Real-world global energy balances must factor in widespread cloud cover, day-night cycles, seasonal variations, and varying solar zenith angles across the entire planet, all of which substantially reduce long-term average surface insolation.

You can read more about the Earth’s average energy balance in my post titled: Global Warming Primer.

Picture: Solar Insolation and Amount Reaching Earth

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Radian and Steradian Defined

Radian (R) Defined

Consider the picture below of a circle of radius r. 

Picture: Radian Defined on a Circle of Radius r

 
It defines the radian R as a unit of angular measurement based on the physical properties of a circle.
 

Radian Definition

An angle (θ) in radians represents the ratio of the circular arc length (L) to the radius (r), defined by the formula: θ = L / r.

 

(RS1) θ (in radians R) = L / r  ; Radian Definition

(RS2) Arc Length L = θr   ; Radian Definition

Understanding the Word ‘Subtend’

The diagram notes that the angle θ is “subtended by” the arc length L.
  • In geometry, to subtend means to “extend under” or “span across.”
  • This means the curved arc along the edge of the circle forms the outer boundary that opens up to create that specific angle at the center.

1 Radian Defined

When the curved arc equals the straight-line radius of the circle (L = r), the angle subtended at the center is exactly 1 radian (approximately 57.3 degrees).

The diagram maps key coordinate thresholds around the circle, showing that a straight line (180 degrees) spans π radians, while a full rotation (360 degrees) spans 2π radians.

Steradian (sr) Defined

Consider the picture below of a sphere with radius r. 

Picture: Steradian Defined on a Sphere of Radius r

A steradian (sr) is the standard unit of measurement for a three-dimensional angle, also known as a solid angle (just means we are dealing with 3D shapes).

  • Just as a regular radian measures an angle along a flat 2D circle, a steradian measures a cone-like angle spreading out through 3D space.

Imagine standing inside the exact center of a hollow sphere with a radius of 1 meter.

  • If you project a beam of light from the center onto the inside wall of that sphere, it will trace out a circular patch.
  • If you expand that beam until the illuminated patch on the wall covers an area of exactly 1 square meter, the angle of that light cone is exactly 1 steradian.
  • If the patch is a circle, then the cone angular spread is defined by the steradian i.e. , the steradian is an angular spread factor
  • For example, 1 steradian defines a cone whose half and full apex angular spreads are 32.74 and 65.5 degrees respectively

The Solid Angle

A solid angle (Ω) represents the ratio of a spherical surface patch area aΩ to the square of the sphere’s radius r², expressed by the formula:
 

(RS3) Ω (in Steradians sr) = aΩ/r² ; Solid Angle (Steradian) Definition

Understanding ‘Subtended’ in 3D

The diagram states that the solid angle Ω is “subtended by” the surface patch area  aΩ.
  • In three dimensions, this means the bounded 2D area patch on the outside of the sphere
  • opens inward to project a cone that forms a specific 3D space angle at the absolute center.
  • A solid angle is equal to 1 steradian (1 sr) when the surface area of the patch equals the radius squared aΩ = r²).
  • At this exact threshold, the projecting cone features a half-apex angle of 32.74 degrees and a total full-apex opening angle of 65.54 degrees.

Total Sphere Space

Because the total surface area of a whole sphere is 4π r², dividing by r² shows that

  • a complete sphere encompasses a total solid angle of exactly 4π steradians or about 12.57 steradians.

Comparison of Steradian and Radian

Think of a steradian as simply the 3D version of a radian.

  • While a flat radian (R) is measured by tracing a curved line along the edge of a circle (θ = L / r  or L = θ r),
  • a volumetric steradian (sr) is measured by tracing a patch of surface area over the shape of a sphere (Ω = A / r² or A =Ωr² ).

An easy way to visualize the scale difference is to look at a complete shape:

  • a flat circle wraps around exactly 2π radians,
  • while a full 3D sphere opens up to encompass a total of 4π steradians.

Picture:  Steradian and Radian Compared

 
 
 

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Projection of Scattered Sunlight on a Sphere Enveloping a Scattering Molecule

Consider the picture below of an atmospheric molecule (e.g. O₂ or N₂) which is receiving sunlight and scattering it outwards.

Picture: Projection of Scattered Sunlight on a Sphere enveloping a Scattering Molecule

 
When incident sunlight strikes a gas molecule (such as N₂ or O₂) at the origin (O), the light oscillates (vibrates or makes it wiggle) the electrons in the molecule, causing it to scatter light in all directions.
 
To measure this scattered light, imagine a large sphere surrounding the molecule and then focus on a tiny, specific patch on its surface, labeled ABCD.
 

Location of a Point on a Spherical Surface

Any point on the spherical surface where scattered light lands is located using spherical coordinates, which consist of:
  • r (Radius): The fixed distance from the center of the sphere.
  • Two angular variables, θ and Φ : The directional angles that pinpoint the exact position on the surface.

The Polar Angle (θ / Theta)

  • This determines the point’s co-latitude (vertical height; see note). An easy way to remember the word latitude is the direction of the “long side” of your mouth when you say the word.
  • It measures the angle downward from the positive vertical Z-axis (0° at the north pole to 180° at the south pole).
  • This angle defines a horizontal (latitudinal) circle (see the picture below also).
  • A changing angle results in vertical movement of that horizontal circle.

Note: Technically, θ measures co-latitude (distance from the North Pole) rather than direct latitude.

  • Latitude measures angle from the equator (-90° +90°), whereas colatitude measures angle from the North Pole (0° to $180°).

The Azimuthal Angle (Φ / Phi):

  • This determines the point’s longitude. An easy way to remember the word is the direction of the “long side” of your mouth when you say the word.
  • It measures the horizontal rotation around the XY-plane (from 0° to 360°).
  • The azimuthal angle defines the exact location the point sits in the horizontal circle defined by the polar angle (see the picture below).

In summary, we can exactly define the location of a point anywhere on a surface of a sphere if we know the radius r, θ and Φ.

In the picture below you can see how
  • the polar angle θ defines the vertical location of a horizontal circle on a sphere.  
  • the azimuthal angle Φ locates a point on the horizontal circle defined by the polar angle.  

Picture: Point Location on a Spherical Surface

 

The Shaded Area Element (ABCD)

Let’s calculate the exact size of the small patch ABCD where the scattered particles land.
 
We look at the lengths of its sides, which are determined by tiny changes in our angles (dθ and dΦ where d implies very small, infinitesimal,  or differential):
 

Picture: Solid Angle Expressed in Spherical Coordinates

 

The Vertical Side (AB = L1 = r dθ)

We know that in a circle, the arc length that subtends an angle θ will equal rθ.

  • (RS2) Arc Length L = θr

So, as the polar angle tilts downward by a tiny differential amount (dθ), it sweeps out a straight physical arc length along a north-south line of longitude equal to: 

  • (PS1) AB = L1 = r dθ

The Horizontal Side (AD = r sinθ dϕ):

  • From the picture above and basic trigonometry,  we know that sinθ = opposite/adjacent = ED/r 
  • So ED = r sinθ, which is the effective radius of the horizontal circle the point lies on. 
  • Using the definition of the circle arc length again (equation RS2) and assuming a tiny differential change in Φ (dΦ),
  • (PS2) AD =  effective radius x dΦ = ED x dΦ = r sinθdΦ.
  • So a tiny horizontal rotation (dΦ) sweeps out a physical arc length equal to r sinθ dΦ.

Area of ABCD

Multiplying these two perpendicular sides gives us the total area of the patch:
  • (PS3) Area = dA =  AB x AD =  (r dθ) × (r sinθ dΦ) = r² sinθ dθ dΦ

Incorporate the Definition of a Solid Angle

Recall that one steradian is the solid angle subtended by any patch of area on a sphere whose total surface area is equal to the square of the radius:
  • (RS3) Ω (in Steradians sr) = aΩ /r²   
or in terms of area:
  • Ωr² = aΩ    

For an infinitesimal area da,

  • dΩr² = daΩ 

Substitute this expression into equation PS3 (the area equation for ABCD), where aΩ = A:

  • (PS4) dΩr² = dA
  • dA = d(AB x AD) = dΩr² =  (r dθ) × (r sinθ dΦ) = r² sinθ dθ dΦ
The r’s cancel and we end up with:
 

(PS5) dΩ = sinθ dθ dΦ ;  Solid Angle in Spherical Coordinates

This is the equation that calculates the exact size of a tiny 3D window (a solid angle element) on the surface of a sphere.

It tells you how a small patch changes in size as you move around a three-dimensional ball. 

  • dΩ: This is the tiny piece of 3D angular space (the solid angle) that you are trying to measure.
  • Think of it as the opening size of a cone projecting from the center of the sphere.
  • dθ: This is a tiny step moving north-to-south.
  • dΦ: This is a tiny step rotating east-to-west.
  • The sinθ Factor: It acts as a scaling corrector—it shrinks the calculated area down near the top and bottom poles

Differential and Total Scattering Cross Section

To calculate how much light goes into that specific patch, physicists use the area element to define the differential scattering cross-section.
  • This gives us the angular “size” of the window ABCD as seen directly from the molecule’s perspective,
  • completely independent of how large or small the imaginary sphere is. 
The differential scattering cross-section acts as the “effective target size” that determines how much incoming light gets deflected into a specific direction.
 
In the previous section, we computed the angular size of area ABCD as seen directly from the molecule’s perspective (completely independent of how large or small the imaginary sphere is).
  • (PS5) dΩ = sinθ dθ dΦ ;  Solid Angle in Spherical Coordinates

Now we’ll define the incoming and outgoing light intensity. 

Incoming Versus Outgoing Light

  • Incident Intensity (Io): The power (energy per second) of the incoming sunlight striking a unit area (in units of W/m²)
  • Outgoing Intensity (I): The power (energy per second) of the outgoing scattered light leaving a unit area (in units of W/m²)
  • Scattered Power (P): The actual amount of light energy per second (in units of Watts) captured inside the area ABCD.
  • Scattered Power (differential) = dP =  Outgoing Intensity (in W/m2) x Area of Patch = (I)(dA)
  • (DS1) dP = IdA ; a differential change in scattering power P.

note: technically, according to radiometric terminology (See Appendix 1 ),  I is irradiance and not intensity, but intensity is commonly used.

We are ready to compute the differential scattering cross section. 

The Differential Scattering Cross-Section 

The differential scattering cross-section area is the ratio of the scattered energy per incoming light intensity. 
  • (DS2) dσ (units of area) = d(Scattered Power)/Incident Intensity = dP/Io 

Substitute equation DS1 (dP = IdA) into DS2: 

  • (DS3) dσ = (I)(dA)/Io

Substitute equation (PS4) dA = dΩr² into (DS3): 

  • dσ = (I)(dΩr²)/Io
  • (DS4) dσ = (I/Io)(r²)(dΩ)

substitute the solid angle definition equation (PS5) dΩ = sinθ dθ dΦ into (DS4):

(DS5) dσ = (I/Io)(r²)(sinθ dθ dΦ) ; Differential Scattering Cross Section

Total Scattering Cross Section

To compute the total scattering cross-section, you perform a double integration of the differential cross-section over all angles of a full sphere,

  • using boundaries from 0 to 2π for the azimuthal (horizontal) angle (Φ) 
  • and 0 to π for the polar (vertical angle θ)

Note, we are essentially expanding that area to cover the full sphere area. We can’t just use the equation of the surface area of a sphere because I is not constant. 

So we have to solve a double integration of equation DS5:   

(DS6) σ = ∫o to 2π∫o to πdσ   , where we integrate through the ranges Φ = 0 to 2π (i.e. , 0 – 3600) and θ = 0 to π (i.e. , 0 – 1800)

Substitute equation (DS5) dσ = (I/Io)(r²)(sinθ dθ dΦ) into (DS6): 

(DS7) σ = ∫o to 2π∫o to π(I/Io)(r²)(sinθ dθ dΦ)

move dΦ to its dedicated integral

(DS8) σ = ∫o to 2π dΦ ∫o to π(I/Io)(r²)(sinθ dθ)

What is this and how do we solve it?

Explaining and Solving the Double Integral

Just as a single integral accumulates a one-dimensional function over a one-dimensional interval (such as the area under a curve), this double integral accumulates a two-dimensional scattering intensity function over the 2D spherical surface of a target, calculating the total effective cross-sectional area σ by summing up scattered particles or light across all possible angular directions.

When you look at a double integral expression like this:

(DS8) σ = ∫o to 2π dΦ ∫o to π(I/Io)(r²)(sinθ dθ)

The easiest way to solve it is to work from the inside out

  • Step 1: Solve the Inside Integral First
  • Focus only on the inner integral sign and its matching variable at the end (in our case, dθ).
  • Treat every other variable in the problem (like Φ) as if it is just a plain, unchanging number.
  • Do your normal calculus integration steps on θ, plug in your upper and lower boundaries (0 and π), and get your result.
  • Step 2: Solve the Outside Integral Second
  • Take the answer you just got from Step 1 and place it inside the remaining outer integral sign, which matches the final variable (dΦ).
  • Now, run your second integration step using your new variable, plug in your remaining boundaries (0 and 2π), and you have your final total value.
  • If the math functions inside the integrals are completely separated i.e. , the θ terms and the Φ terms are multiplied together rather than added,
  • you can split the double integral completely apart into two independent single integrals.
  • You simply calculate the answer to both individual pieces separately and multiply the two results together at the end!

Solving the Integral: Setting Up the Substitution

For I/Io we’ll use the Rayleigh equation
  • Recall out general relationship for Rayleigh Scattering in equation SA1  :
  • (SA1) I ∝ (Io)(1/λ⁴ )(1+cos²θ)  
  • A more accurate equation is shown below.
  • The intensity of light scattered by any one of the small spheres of radius r (or diameter 2r) and refractive index n (see Appendix 2) from a beam of unpolarized light of wavelength λ and intensity Io is given by

(DS9) I / Io = [ (1 + cos²θ) / (2r²) ] × (2π / λ)⁴ × [ (n² – 1) / (n² + 2) ]² × (d / 2)⁶ ; Rayleigh Equation

  • where r is the observer’s distance to the particle and θ is the scattering angle

Note: Almost all common light sources—like the sun, standard incandescent light bulbs, and candles—emit unpolarized light. Because its electric fields are randomly pointing in all directions around the beam’s axis,  unpolarized light has no “up-down” or “left-right” bias.

To make the integration clean, group all the constant terms into a single constant symbol, C:
  • (DS10) C = (1 / 2) × (2π / λ)⁴ × [ (n² – 1) / (n² + 2) ]² × (d / 2)⁶

The intensity ratio equation (DS9) now looks a lot less cluttered when we substitute in C. 

  • (DS11) I / I0 = C × (1 + cos²θ) / r²

Solving the Integral: Plugging I/I0 into the Total Cross-Section Integral

Now we substitute DS11 into the double integral formula DS8:
  • (DS8) σ = ∫0 to 2π dΦ ∫0 to π (I / Io) × r² × sinθ dθ
  • (DS12) σ = ∫0 to 2πdΦ ∫0 to π[ C × (1 + cos²θ) / r² ] × r² × sinθ dθ
The r²s cancel out and we can move C out of the integral
  • (DS13) σ =C ∫0 to 2πdΦ ∫0 to π(1 + cos²θ)sinθ dθ

Part 1: Solving the Integral: The Φ Integral (Horizontal Rotation)

Since there are no variables inside this part, it simply integrates to the length of the interval:
  • (DS14) ∫0 to 2πdΦ = 2π

Part 2: Solving the Integral: The θ Integral (Vertical Angle)

To evaluate ∫0 to π(1 + cos²θ)sinθ dθ we use the u-substitution method:
  • Let u = cosθ
  • Then the derivative is du = -sinθ dθ, which means sinθ dθ = -du
  • Change the integration boundaries using u = cosθ
  • When θ = 0, u = cos(0) = 1
  • When θ = π, u = cos(π) = -1
  • Substitute u and -du into the integral
  • ∫1 to -1 (1 + u²) (-du)
  • Flip the boundaries to remove the negative sign 
  • ∫-1 to 1(1 + u²) (-du) = ∫(-1 to 1) (1 + u²) du
  • Find the antiderivative
  • ∫-1 to 1(1 + u²) du = [ u + (u³ / 3) ] evaluated from -1 to 1
  • Plug in the upper boundary (1) and subtract the lower boundary (-1)
  • (DS15) ∫-1 to 1(1 + u²) du = [ 1 + (1/3) ] – [ -1 + (-1/3) ] = [ 4/3 ] – [ -4/3 ] = 8/3

Part 3: Solving the Integral: Combining the Final Terms

Now we multiply all of our solved pieces back together (Constant C × DS14 × DS15):
  • σ = C × 2π × (8/3)
  • (DS16) σ = (16π / 3) × C
Finally, plug the expression for C  (Equation DS10) back into DS16:
  • (DS17) σ = (16π / 3) × (1 / 2) × (2π / λ)⁴ × [ (n² – 1) / (n² + 2) ]² × (d / 2)⁶
Simplify the front fractions (16π/3) × (1/2) = (8π/3) 
  • (DS18) σ = (8π / 3) × (2π / λ)⁴ × [ (n² – 1) / (n² + 2) ]² × (d / 2)⁶
Expand the wavelength term:
  • (DS19): (2π / λ)⁴ = (2⁴ × π⁴) / λ⁴ = 16π⁴ / λ⁴

Expand the molecular diameter term: 

  • (DS20): (d / 2)⁶ = d⁶ / 2⁶ = d⁶ / 64
Substitute the above expanded terms (DS19, DS20)  back into the main equation DS18:
  • (DS21) σ = (8π / 3) × (16π⁴ / λ⁴) × [ (n² – 1) / (n² + 2) ]² × (d⁶ / 64)
Next, group all the standalone numerical fractions and powers of π together at the front of the equation:
  • Numerator coefficients: 8 × 16 = 128
  • Denominator coefficients: 3 × 64 = 192
  • Combining the numbers: 128 / 192 = 2 / 3
  • Combining the π terms: π × π⁴ = π⁵
Replacing the constants with our simplified values, DS21 becomes:
  • (DS22) σ = (2/3) × (π⁵ / λ⁴) × d⁶ × [ (n² – 1) / (n² + 2) ]²
The Final Standard Equation (Version 1)
 

(DS23) σ = [ (2π⁵ d⁶) / (3λ⁴) ] × [ (n² – 1) / (n² + 2) ]² ; V1: Rayleigh Total Scattering Cross-Section formula – particle diameter based

Expressed in terms of r instead of d (d = 2r for particle) and using exponent rules:

  • σ = [ (2π⁵ (2r)⁶) / (3λ⁴) ] × [ (n² – 1) / (n² + 2) ]²
  • σ = [ (2π⁵ 2⁶r⁶) / (3λ⁴) ] × [ (n² – 1) / (n² + 2) ]²
  • σ = [ (π⁵21 2⁶r⁶) / (3λ⁴) ] × [ (n² – 1) / (n² + 2) ]²
  • σ = [ (π⁵23 24r⁶) / (3λ⁴) ] × [ (n² – 1) / (n² + 2) ]²
  • σ = [ (π⁵23 24r⁶) / (3λ⁴) ] × [ (n² – 1) / (n² + 2) ]²
  • σ = [ (π1π42324r⁶) / (3λ⁴) ] × [ (n² – 1) / (n² + 2) ]²
  • σ = [ (π1π42324r⁶) / (3λ⁴) ] × [ (n² – 1) / (n² + 2) ]²
  • σ = [ 1/3(23π1π4)(24/λ⁴) ] × [ (n² – 1) / (n² + 2) ]²× r⁶
  • σ =  (8π/3)(24π4/λ⁴) × [ (n² – 1) / (n² + 2) ]² × r⁶

So DS23 can also be expressed as

(DS24) σ =  (8π/3)(2π/λ)4  × [(n² – 1)/(n² + 2)]²  × r⁶; V2: Rayleigh Total Scattering Cross-Section formula – particle radius based

This equation tells us that in Rayleigh scattering:

  • the total amount of scattered light is inversely proportional to the fourth power of the wavelength (1/λ⁴).
  • Les assume we have blue light at 450nm being scattered and red light at 700 nm being scattered.
  • σblue;450nm /σred;700nm   = (λred;700nm/λblue;450nm)4   = (700/450)4  = 5.8
  • So Blue Light at 450 nm scatters about 6x as much as red light.

Why the sky is blue during the day

During the middle of the day, sunlight enters the atmosphere from overhead and takes a short, direct path to your eyes.

  • The steep 1/λ⁴ drop-off means shorter blue wavelengths interact with air molecules much more aggressively than longer wavelengths, scattering blue light in every direction across the sky while red light passes through relatively undisturbed.

Why we see orange/red at sunsets and sunrises

At sunrise and sunset, when the sun is low on the horizon, sunlight must travel through a much thicker layer of the atmosphere to reach you.

As shown in the picture below,  the distance of sunlight to an observer at sunrise Lmax can be 38x further than it is when the sun is straight overhead at Lmin. 

Picture:  Solar Zenith Angle 

  • Because of this longer path, almost all of the blue light is scattered away in other directions long before it reaches your line of sight.
  • What remains to pass straight through this heavy atmospheric filter are the longer, less easily scattered red and orange wavelengths.

Picture: Blue Scatter Above But Only Orange/Red Gets Through along the Horizon

 

Why do we See Blue more than Purple?

The reason we see blue instead of purple when looking at the sky or a rainbow comes down to two main factors:

  • solar emission output and
  • human eye photoreceptor sensitivity.

While Rayleigh scattering dictates that shorter wavelengths scatter much more efficiently than longer ones (scaling inversely with the fourth power of wavelength, 1/λ⁴, two things happen at the extreme short end of the visible spectrum:

  • The Sun emits less violet light: The sun’s radiation curve drops off significantly in the ultraviolet and deep violet range compared to its peak output in the blue and green regions.

Picture: Solar Spectrum at Top of Earth Atmosphere and at Sea Level

  • Human color perception: Our eyes have three types of color-sensing cone cells (red, green, and blue).
  • Violet light stimulates both the short-wavelength (blue) cones and—to a lesser extent—the long-wavelength (red) cones.
  • Combined with our lower sensitivity to light wavelengths below 450 nm, our brain perceives the mix of scattered short-wavelength light predominantly as sky-blue rather than pure violet.

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Molecules as Equivalent Spherical Particles (Number Density)

There are a few more ways to write the Rayleigh Total Scattering Cross-Section Formula. 
  • We’ll need these to develop % scattering plots in the next section.
  • We need to convert the formula into something that directly incorporates the non spherical nature of the molecules in the atmosphere.  
If you want to treat a molecule like nitrogen or oxygen as an equivalent spherical particle, you can estimate its effective radius by looking at the average volume available to each molecule. 
 
The number density (N) of a molecule is the number of particles per unit volume. 
  • (SP1) N = # particles/unit volume
  • (SP2) So the reciprocal 1/N = the average volume occupied by a single molecule = Vmolecule 

So, let Vmolecule  reflect the volume of a sphere (where V = 4/3 πr3).

  • (SP3) Vmolecule = 4/3 πr3

Now, find an expression for the effective radius (r) of this molecule modelled as a sphere. 

Using equations SP2 and SP3:

  • (SP4) Vmolecule  =  (4/3) πr3 = 1/N

Re-arrange:

  • (SP5) r3 = 3/(4πN)

Express this as r6 to make it consistent with our scattering equation.  

  • (SP6) r6 = (r3)2=  [3/(4πN)]2 = 9/(16 π2N2)

Recall the Rayleigh Total Scattering Cross Section Formula:

  • (DS24) σ =  (8π/3)(2π/λ)4  × [(n² – 1)/(n² + 2)]²  × r⁶; V2: Rayleigh Total Scattering Cross-Section formula

Substitute for r6 (equation SP6) in equation DS24 and organize the terms:

  • σ =  (8π/3)(2π/λ)4  × [(n² – 1)/(n² + 2)]²  × 9/(16 π2N2)
  • σ =  (8π/3)(16π4/λ4)  ×  9/(16 π2N2)  × [(n² – 1)/(n² + 2)]²  
  • σ =  [(8×16×9)/(3 × 16 )] ×  (π × π4/π2)  ×  1/( λ4N2)  × [(n² – 1)/(n² + 2)]² 
  • σ =  [(8×16×9)/(3 × 16 )] ×  (π × π4/π2)  ×  1/( λ4N2)  × [(n² – 1)/(n² + 2)]² 
  • σ =  24 ×  π3  ×  1/( λ4N2)  × [(n² – 1)/(n² + 2)]² 

(SP7) σ =  (24π3 )/( λ4N2)  × [(n² – 1)/(n² + 2)]² ; V3: Rayleigh Total Scattering Cross-Section formula – Number density (Molecule) based

Real atmospheric gases (like nitrogen N2 and oxygen O2 ) consist of non-spherical, anisotropic molecules rather than perfect isotropic spheres.

  • In scattering, the difference between isotropic and anisotropic tells you whether a particle bounces off a target randomly (isotropic) in any direction or prefers a specific direction (anisotropic).

To account for this, atmospheric physicists multiply the final expression by the King Correction Factor (Fk). [see this NIH article]

  • For Spherical / Monoatomic Gases: (such as Helium or Argon) Fk = 1.
  • Anisotropic Gases: For linear or polyatomic molecules (such as Nitrogen or Carbon Dioxide), Fk > 1.
  • Typical Values: In the visible and near-ultraviolet spectrum, Fk values are typically close to unity but slightly elevated: Fk  ≈  1.03 to 1.06 for standard atmospheric gases like air and nitrogen.

So we end up with a useful form of the Rayleigh Scattering Cross Section Formula that we can use to do Percent Scattering calculations. 

(SP8) σ =  (24π3 )/( λ4N2)  × [(n² – 1)/(n² + 2)]² × Fk  ; V4: Rayleigh Total Scattering Cross-Section formula – Number density (Molecule) based – anisotropy corrected

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Percent Scattering Equations

If you do a web search on “Rayleigh Scattering” you will probably find the picture below.

Picture: Percent Scattering of Direct Sunlight (Rayleigh Scattering)

It plots percent scattering of direct sunlight against wavelength along the visible spectrum. 
  • Vertical columns of color allow you to match wavelength to color. 
  • So this says that about 23% of very short wavelength visible light (400 nm) is scattered
  • while about 4% of 650 nm red light is scattered.   

Note that this graph assumes a straight overhead position of the sun (i.e. , sun rays are going through the narrowest distance of atmosphere to the earth).

It would be nice to see how the curve changes with changing position of the sun in the sky.

In order to generate a multi-curve % scattering plot for various positions of the sun in the atmosphere, we need a few more equations. 

1. Rayleigh Scattering Coefficient (β)

The Rayleigh Scattering Coefficient, β,  Measures the fraction of light intensity lost to scattering per unit distance as a beam travels through a gas.

It’s unit of measure is 1/m (or m-1  = inverse meters)

  • (SE1) β = N · σ 

Substitute in our expression for σ (equation SP8): 

  • (SE2) β = N (24π3 )/( λ4N2)  × [(n² – 1)/(n² + 2)]² × Fk

Combine the N terms:

(SE3) β = (24π3)/( λ4N)  × [(n² – 1)/(n² + 2)]² × Fk ; Rayleigh Scattering Coefficient

where
  • N: Molecular density
  • n: Refractive index  (see Appendix 2)
  • [(n² – 1)/(n² + 2)]² :  a term that accounts for polarizability  (see Appendix 2)
  • Fk: King correction factor

2. The Beer-Lambert Law for Transmission

The fraction of light that successfully transmits through the atmosphere without being scattered away is:
 

(SE4) T = exp(-τ); Beer-Lambert Law for Transmission

Where
  • τ is the total optical depth of the atmosphere at wavelength λ.
  • T = Transmittance
You may be more familiar with the Beer-Lambert law written as
  • (SE5) A = εcl. 
where
  • A : Absorbance
  • ɛ: Attenuation Coefficient: Molar Absorption Coefficient 
  • C: Molar Concentration 
  • L: Optical Path Length 
Let’s convert this into equation SE4 to show its the same thing.
 
In physics and atmospheric science, the Beer-Lambert law is frequently expressed using the natural logarithm where absorbance is defined as
  • (SE6) A = -ln(T).
Substitute equation SE6 into equation SE5
  • (SE7) – ln(T) = εcl
Define the optical density (or optical depth) as the product of the attenuation coefficient, concentration, and path length:
  • (SE8) τ = εcl
So equation SE7 becomes:
  • (SE9) – ln(T) = τ
  • (SE10) ln(T) = – τ

Take the exponent of both sides of equation SE9:

  • (SE11) T = exp(- τ) 
3. Optical Depth (τ) with Kasten-Young Airmass (AM)
Optical depth scales with the path length through the atmosphere, represented by the airmass AM:
 

(SE12) τ = β × H × AM ; Optical Depth

  • H: Scale height of the atmosphere (~ 8,400 meters).
  • AM: The Kasten-Young airmass formula, which depends on the solar zenith angle (θz).

4. Kasten-Young Airmass Formula (AM)

For a given apparent solar zenith angle θz (in degrees), the airmass AM is calculated as:
 

(SE13) AM = 1 / [cos(θz) + 0.50572 × (96.07995 – θz) – 1.6364]

Note in the picture below how the AM values are highest (AM = 38) at sunrise and sunset when L is at Lmax (indicating “thickness of atmosphere”).

This coincides with sunrise and sunset zenith angles θz of 90 degrees. 

Picture:  Solar Zenith Angle and AM Values for Houston Texas in July

 

Let’s use these four equations to generate % scattering curves for visible light at different AM values (i.e. , different locations in the sky relative to an observer). 

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Atmospheric Light Scattering Calculations

Example Calculation To Compute Percent Scattering of Sunlight

  • Purple/Blue light at λ=400 nm
  • for both AM=1.96 (about 9 am in Houston in July) and AM=3.26 (about 8am in Houston in July).

Known Values

  • Wavelength λ: 400 nm=4.0×10-7 m
  • AM=1.96 and AM=3.26
  • Molecular Number Density (N): 2.547×1025 molecules/m3
  • Effective Scale Height (H): 8,400 m
  • King Correction Factor (Fk): 1.048

Compute the n term in the equation SE3 (Rayleigh Scattering Coefficient).

  • Assume a refractive index of air of n = 1.000278, which is the standard value for air specifically at a wavelength of 400 nm. 
  • n doesn’t change significantly with visible wavelength so we will keep it constant.
  • ((n2-1)/(n2+2))2  ≈ 3.552×10-8

Compute the Rayleigh Scattering Coefficient β (Equation SE3): 

  • (SE3) β =(24π3)/(λ4 N) × ((n2-1)/(n2+2))2 × Fk
  • Denominator term (λ4 N): (4.0×10-7)4 × (2.547×1025) = (2.56×10-26)×(2.547×1025) = 0.65203 m
  • β =(744.38/0.65203)×(3.552×10-8) × 1.048
  • β = 4.25×10-5 m-1

 Calculate optical depth τ for AM = 1.96.

  • (SE12) τ = β×H×AM
  • τ = (4.25×10-5 m-1)⋅(8,400 m ) × 1.96
  • τ = 0.700

Compute the Beer-Lambert Transmission (T) for AM = 1.96.

  • (SE4) T = exp(-τ)
  • T = e-.7 ≈ 0.4966 (49.7%  reaches the surface )

Compute Percent Blue Light Scattered for AM = 1.96.

  • Scattered = (1 – 0.4966)×100 = 50.3%

Calculate τ for AM = 3.26.

  • τ = β x H x AM
  • τ = 4.25×10-5 m-1  x  8,400 x 3.26 = 1.164

Compute Beer-Lambert Transmission (T) for AM = 3.26. 

  • (SE4) T = exp(-τ)
  • T = e-1.164 ≈ 0.3122 (31.2% reaches the surface )

Compute Percent Blue Light Scattered for AM = 3.26.

  • Scattered = (1 – 0.3122)×100 = 68.8%

Summary for 400 nm Purple/Blue Light

  • At AM = 1.96 (about 9am in Houston in July) :  τ=0.700 → 50.3% of the light is scattered out of the direct incident beam.
  • At AM = 3.26 (about 8am in Houston in July)  : τ=1.164 → 68.8% of the light is scattered out of the direct incident beam.

Atmospheric Light Scattering Curves at Various AM Values 

OK, so I did the calculations for various AM (atmospheric depth) values for Houston Tx in the summer and charted them in the picture below. 

Picture: Atmospheric Light Scattering Curves (Houston Tx in the Summer)

This graph illustrates atmospheric light scattering percentages across the visible light spectrum (400 – 700 nm) as calculated using the Rayleigh scattering equation, the Beer-Lambert law, and Kasten-Young airmass profiles for summer solar angles in Houston, Texas.

It shows a family of curves showing that scattering intensity increases markedly at shorter wavelengths (toward the violet and blue end) and higher air mass values (ranging from AM = 1.01 at 1:25 pm up to AM = 6 at 7:30 am), which causes greater attenuation when the sun is lower on the horizon.

Regarding Ultraviolet light:

  • UV-C (100–280 nm): Completely absent from ground-level observation due to total upper-atmosphere stratospheric shielding (oxygen and ozone).
  • UV-B (280–315 nm): Experiences severe attenuation at high air mass (AM > 3) because ozone absorption compounds with heavy scattering.
  • UV-A (315–400 nm): The longest UV wavelengths. Deeply penetrating, minimally blocked by ozone, and moderated primarily by Rayleigh scattering—making up the bulk of the gentle UV dosage you experience during a morning walk

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Appendix 1 – Flux , Exitance (Emittance), Radiance, Irradiance, and Intensity

Light energy can be expressed in different ways.  

Radiant Flux

Radiant Flux,  Φe , is the total power coming off a source in all directions.

Power is Energy/time. Has SI units of  Joules/second = Watts = W. 

Picture: Radiant Flux

Radiant Exitance (or Emittance)

  • It is the total energy leaving a surface in all directions, broken down by wavelength.
  • The radiant (luminous) exitance is the energy per unit area leaving a surface.
  • Imagine standing back and measuring every single photon flying off a flat glowing plate into the entire hemisphere above it.
  • Unit of measure: Power per unit area (W / m²) but can be expressed also  per wavelength (W / m² / m). 
  • It ignores direction; it just asks, “How much total power is pouring out of this patch of surface?”

Picture: Exitance

   

Radiance

  • Radiance is the directional view: power leaving a surface per unit area, per solid angle (steradian; see  wuz), and per wavelength.
  • We could call it the surface radiance also: the surface radiance (luminance) is the intensity per unit area leaving a surface.
  • Instead of looking at the whole hemisphere, you zoom in on one specific “dot” on the surface and look at it from one precise angle through a narrow cone of sight.
  • Units of measure: W / (m² x sr ) or sometimes expressed per wavelength as  W / (m² x sr x m)
  • Radiance accounts for geometry and directionality. 

Picture: Radiance

Irradiance: Inverse-Square Law Relationship (I = P / 4π r²)

  • This calculates irradiance  (or sometimes called flux density), not radiance.
  • Be aware that very often engineers and physicists will call this wave intensity or solar intensity which technically is not consistent with common radiometry terms. 
  • The irradiance (illuminance) is the power per unit area incident on a surface.
  • You take the Sun’s total output power (P), and spread it out over the surface area of an expanding imaginary sphere of radius r (4π r²) centered on the Sun.
  • When that energy hits Earth, you are calculating how much power is arriving per unit area.
  • Units of measure: Power per unit area (W / m²). 

Picture: Irradiance

 

Be Careful When you use the word Intensity

Be aware that people will call P / (4π r²) “wave intensity” or “solar intensity.”

But in strict radiometry terminology,

  • power received by a surface is irradiance (Watts/m²),
  • while power emitted from a point source per solid angle is radiant intensity (W/sr).

Picture: Radiant Intensity

Summary

Radiance: Directional brightness from a specific patch at a specific angle (W / (m² x sr)). 

Radiant Exitance (Emittance): Total light pouring out of a surface in all directions (W / m²).

Irradiance: Inverse-Square Calculation (I = P / 4π r² ):  How much total power is hitting a square meter out at distance r (W / m²).

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Appendix 2 – Refractive Index and Polarizability

I used Google Gemini to write this section. 

Refractive Index

The refractive index (usually written as n) of a substance measures how much it bends (refracts) and slows down light as the light wave passes through it compared to how fast it travels in a vacuum.

See my article on Snell’s Law. 

For example, a refractive index of n = 1.5 means that light travels 1.5 times slower inside that substance than it does in a vacuum.

Lorentz-Lorenz Relation

The Lorentz-Lorenz relation (also known as the Clausius-Mossotti relation in electrostatics) is an equation that connects the macroscopic refractive index () of a substance to its microscopic molecular polarizability () and number density ().

  • (n2−1)/(n2+2)​=Nα/​3ϵo
  • : Refractive index (macroscopic)
  • : Number density of molecules per unit volume
  • : Molecular polarizability (how easily an electron cloud distorts in an electric field)
  • ϵo: Permittivity of free space

Why does it matter in Rayleigh scattering?

Recall the Rayleigh Scattering Coefficient equation:

  • (SE3) β = (24π3)/( λ4N)  × [(n² – 1)/(n² + 2)]² × Fk ; Rayleigh Scattering Coefficient

The refractive index n plays a very precise role in the equation. 

  • The Inner Term (n² – 1)/(n² + 2) : The Lorentz-Lorenz relation relates n to the effective polarizability of the individual molecules.
  • The entire fraction is squared,  [(n² – 1)/(n² + 2)]² ,  because the physical intensity of Rayleigh scattering is proportional to the square of the molecular

Polarizability

Think of an air molecule (like nitrogen, oxygen, or argon) as a tiny ball with a positive center (the nucleus) surrounded by a cloud of negative charges (electrons).

  • Polarizability is simply a measure of how stretchy or “wiggly” a molecule’s electron cloud is when an electric field hits it.
  • If a molecule has a high polarizability, its electrons are loosely held and easy to push around. If it has a low polarizability, its electrons are tightly locked down and hard to budge.

Refractive Index of Air

While the refractive index (n) varies slightly across the visible spectrum, its impact is heavily dwarfed by the λ2, which single-handedly drives the primary wavelength-dependent drop in scattering.

If you do want to account for wavelength-specific variations in n for high-precision modeling, you can use the standard Edlén equation for dry air.

If you just want a reliable average value for standard conditions (sea-level pressure, room temperature, and visible light), you can use:

  • n = 1.00029

This is the standard approximation for dry air in the visible spectrum and introduces negligible error for most general scattering calculations.

Nitrogen, Oxygen, and Argon

  • Nitrogen and Oxygen make up 99% of our air.
  • Their electron clouds have a moderate, steady “stretchiness” (polarizability).
  • Argon is a single atom rather than a pair, but it shares a similar electron response.
  • When light hits them, this refractive index ratio dictates how hard their electron clouds wiggle, constantly bouncing and scattering short wavelengths (like blue light) all over the sky!

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Appendix 3 – Integral as Continuous Accumulator

At every level of mathematics, an integral is fundamentally a universal accounting engine for continuous accumulation.

It does one thing and one thing only:

  • It takes a space,
  • chops it into infinitesimal building blocks,
  • multiplies each block by a weight, and
  • adds them all up.

Every single integral is just a formal limit of a Riemann sum:

Total Accumulation = limit “mesh” →0⁡∑i Weighti × Infinitesimal Chunki ; Integral General Definition

  • mesh = largest chunk

As you make your chunks infinitely small, the sum becomes an integral ∫, a shorthand for S = sum.  

Every integral you will ever encounter in physics, math, or engineering is built from three exact components:

  • The Domain: The space you are covering (a line, a surface, or a volume).
  • The Infinitesimal Chunk (dx,dA,dV): The geometry element that defines the true size of your building block in that specific coordinate system.
  • The Weight (f): What you actually want to multiply each chunk by. (If you want pure unweighted size, the weight is just 1).

1. The Single Integral (1D Accumulation)

What it is: Accumulating a quantity distributed along a one-dimensional path or interval.

∫a to b (Weight) x (Length Chunk) = ∫a to b f(x)dx  

  • The Domain (a to b): A straight line or a path from point a to point b.
  • The Chunk (dx): An infinitesimal slice of length.
  • The Weight (f(x)): Whatever value you are tracking at point x.

Regarding the Weight 

  • If weight = 1: You are just adding up lengths → Total Distance.
  • Area Under a Curve: When the weight is set to a height function (f(x)), the engine multiplies a 1D length chunk (dx) by a vertical height (f(x)). This turns every infinitesimal slice into a thin rectangular column (width x height), accumulating into total 2D area.
  • If weight = Velocity (v(t)), you get total distance traveled.
  • If weight = Linear density ρ(x), you get total mass of a wire.

2. The Double Integral (2D Accumulation)

What it is: Accumulating a quantity distributed across a two-dimensional surface or region.

∬R Weight x Area/Surface Chunk =∬R f(x,y) x dA 

  • The Domain (R): A 2D flat floor, a curved shell, or a parameter space (like angles on a sphere).
  • The Chunk (dA): An infinitesimal patch of surface area.

The Chunk (dA): Its exact mathematical recipe depends on your coordinate system

  • Flat Cartesian: dA=dx dy
  • Curved Spherical: dA=R2sin⁡(θ) dθ dΦ

The Weight f(x,y): What you multiply each surface patch by

  • Volume Under a Surface: When the weight is set to a height function (f(x,y)) in Cartesian coordinates, the engine multiplies a flat 2D area patch (dxdy) by a vertical height (f(x,y)). This turns every infinitesimal patch into a thin rectangular column (base area x height), accumulating into total 3D volume.
  • If weight = 1: You are adding up pure area patches → Surface Area.
  • If weight = Surface density: You are multiplying area by mass-per-area → Total Mass of a Sheet.
  • If weight = Scattering intensity function: You are multiplying sky patches by bounce probability → Total Scattering Cross-Section.

3. The Triple Integral (3D Accumulation)

What it is: Accumulating a quantity distributed throughout a three-dimensional volume.

∫∫∫ V  Weight x Volume Chunk =∫∫∫ V f(x,y,z) x dV

  • The Domain (V): A solid 3D space (a block, a sphere, a star).
  • The Chunk (dV): An infinitesimal brick of 3D volume.

DV recipe changes based on coordinates:

  • Flat Cartesian: dV=dx dy dz
  • Cylindrical: dV=r dr dθ dz
  • Spherical: dV=ρ2 sin⁡(θ) dρ dθ dΦ

The Weight (f(x,y,z)): What you multiply each 3D brick by.

  • If weight = 1: You are adding up pure volume bricks → Total Volume.
  • If weight = 3D Mass Density (ρ): You are multiplying volume bricks by density → Total Mass of a Solid Object.
  • If weight = Temperature/Charge density: You are tracking thermal energy or electrical charge distributed across space.

Summary

When you integrate:

  • Choose your dimension (1D line, 2D surface, 3D space).
  • Pick your coordinate system so your geometry chunks (dx,dA,dV) correctly account for whether space is flat, stretching, or curving.
  • Set your weight (f).
  • Set (f) to 1 if you just want to know the raw size of the space (Length, Area, Volume).
  • Set (f) to anything else (Density, Probability, Velocity, Intensity) if you want to accumulate a physical quantity distributed across that space.

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