Limits of Resolution: The Rayleigh Criterion

Light diffracts as it moves through space, bending around obstacles, interfering constructively and destructively. While this can be used as a spectroscopic tool—a diffraction grating disperses light according to wavelength, for example, and is used to produce spectra—diffraction also limits the detail we can obtain in images. [Figure 1](a) shows the effect of passing light through a small circular aperture. Instead of a bright spot with sharp edges, a spot with a fuzzy edge surrounded by circles of light is obtained. This pattern is caused by diffraction similar to that produced by a single slit. Light from different parts of the circular aperture interferes constructively and destructively. The effect is most noticeable when the aperture is small, but the effect is there for large apertures, too.

Part a of the figure shows a single circular spot of bright light; the light is dimmer around the edges. Part b of the figure shows two circles of light barely overlapping, forming a figure eight; the dimmer light surrounds the outer edges of the figure eight, but is slightly brighter where the two circles intersect. Part c of the figure shows two circles of light almost completely overlapping; again the dimmer light surrounds the edges but is slightly brighter where the two circles intersect.

How does diffraction affect the detail that can be observed when light passes through an aperture? [Figure 1](b) shows the diffraction pattern produced by two point light sources that are close to one another. The pattern is similar to that for a single point source, and it is just barely possible to tell that there are two light sources rather than one. If they were closer together, as in [Figure 1](c), we could not distinguish them, thus limiting the detail or resolution we can obtain. This limit is an inescapable consequence of the wave nature of light.

There are many situations in which diffraction limits the resolution. The acuity of our vision is limited because light passes through the pupil, the circular aperture of our eye. Be aware that the diffraction-like spreading of light is due to the limited diameter of a light beam, not the interaction with an aperture. Thus light passing through a lens with a diameter $D$ shows this effect and spreads, blurring the image, just as light passing through an aperture of diameter $D$ does. So diffraction limits the resolution of any system having a lens or mirror. Telescopes are also limited by diffraction, because of the finite diameter $D$ of their primary mirror.

Take-Home Experiment: Resolution of the Eye

Draw two lines on a white sheet of paper (several mm apart). How far away can you be and still distinguish the two lines? What does this tell you about the size of the eye’s pupil? Can you be quantitative? (The size of an adult’s pupil is discussed in Physics of the Eye.)

Just what is the limit? To answer that question, consider the diffraction pattern for a circular aperture, which has a central maximum that is wider and brighter than the maxima surrounding it (similar to a slit) [see [Figure 2](a)]. It can be shown that, for a circular aperture of diameter $D$ , the first minimum in the diffraction pattern occurs at $\theta =1.22 \lambda /D$ (providing the aperture is large compared with the wavelength of light, which is the case for most optical instruments). The accepted criterion for determining the diffraction limit to resolution based on this angle was developed by Lord Rayleigh in the 19th century. The Rayleigh criterion for the diffraction limit to resolution states that two images are just resolvable when the center of the diffraction pattern of one is directly over the first minimum of the diffraction pattern of the other. See [Figure 2](b). The first minimum is at an angle of $\theta =1.22 \lambda /D$ , so that two point objects are just resolvable if they are separated by the angle

$$\theta =1.22\frac{\lambda }{D}, $$

where $\lambda$ is the wavelength of light (or other electromagnetic radiation) and $D$ is the diameter of the aperture, lens, mirror, etc., with which the two objects are observed. In this expression, $\theta$ has units of radians.

Part a of the figure shows a graph of intensity versus theta. The curve has a central maximum at theta equals zero and its first minima occur at plus one point two two lambda over D and minus one point two two lambda over D. Farther from the central peak, several small peaks occur, but they are much much smaller than the central maximum. Part b of the figure shows a drawing in which two light bulbs, labeled object one and object two, appear in the foreground positioned next to each other. Two rays of light, one from each light bulb, pass through a pinhole aperture and continue on to strike a screen that is farther back in the drawing. On the screen is an x y plot of the two resulting intensity patterns. Because the rays cross in the pinhole, the ray from the left light bulb makes the right-hand intensity pattern, and vice versa. The angle between the rays coming from the light bulbs is labeled theta min. Each ray hits the screen at the central maximum of the intensity pattern that corresponds to the object from which the ray came. The central maximum of object one is at the same position as the first minimum of object two, and vice versa.

Connections: Limits to Knowledge

All attempts to observe the size and shape of objects are limited by the wavelength of the probe. Even the small wavelength of light prohibits exact precision. When extremely small wavelength probes as with an electron microscope are used, the system is disturbed, still limiting our knowledge, much as making an electrical measurement alters a circuit. Heisenberg’s uncertainty principle asserts that this limit is fundamental and inescapable, as we shall see in quantum mechanics.

Calculating Diffraction Limits of the Hubble Space Telescope

The primary mirror of the orbiting Hubble Space Telescope has a diameter of 2.40 m. Being in orbit, this telescope avoids the degrading effects of atmospheric distortion on its resolution. (a) What is the angle between two just-resolvable point light sources (perhaps two stars)? Assume an average light wavelength of 550 nm. (b) If these two stars are at the 2 million light year distance of the Andromeda galaxy, how close together can they be and still be resolved? (A light year, or ly, is the distance light travels in 1 year.)

Strategy

The Rayleigh criterion stated in the equation $\theta =1.22\frac{\lambda }{D}$ gives the smallest possible angle $\theta$ ** between point sources, or the best obtainable resolution. Once this angle is found, the distance between stars can be calculated, since we are given how far away they are.

Solution for (a)

The Rayleigh criterion for the minimum resolvable angle is

$$\theta =1.22\frac{\lambda }{D}. $$

Entering known values gives

$$\begin{array}{}\theta =1.22\frac{550 \times 10^{-9} \text{m}}{2.40 \text{m}}\\ = 2.80 \times 10^{-7} \text{rad} \text{.} \end{array} $$

Solution for (b)

The distance $s$ between two objects a distance $r$ away and separated by an angle $\theta$ is $s= r\theta$.

Substituting known values gives

$$\begin{array}{lll}s& =& \left( 2.0 \times 10^{6} \text{ly}\right)\left( 2.80 \times 10^{-7} \text{rad}\right)\\ s & =& 0.56\text{ ly.}\end{array} $$

Discussion

The angle found in part (a) is extraordinarily small (less than 1/50 000 of a degree), because the primary mirror is so large compared with the wavelength of light. As noticed, diffraction effects are most noticeable when light interacts with objects having sizes on the order of the wavelength of light. However, the effect is still there, and there is a diffraction limit to what is observable. The actual resolution of the Hubble Telescope is not quite as good as that found here. As with all instruments, there are other effects, such as non-uniformities in mirrors or aberrations in lenses that further limit resolution. However, [Figure 3] gives an indication of the extent of the detail observable with the Hubble because of its size and quality and especially because it is above the Earth’s atmosphere.

Two pictures of the same galaxy taken by different telescopes are shown side by side. Photo a was taken with a ground-based telescope. It is quite blurry and black and white. Photo b was taken with the Hubble Space Telescope. It shows much more detail, including what looks like a gas cloud in front of the galaxy, and is in color.

The answer in part (b) indicates that two stars separated by about half a light year can be resolved. The average distance between stars in a galaxy is on the order of 5 light years in the outer parts and about 1 light year near the galactic center. Therefore, the Hubble can resolve most of the individual stars in Andromeda galaxy, even though it lies at such a huge distance that its light takes 2 million years for its light to reach us. [Figure 4] shows another mirror used to observe radio waves from outer space.

The figure shows a photograph from above looking into the Arecibo Telescope in Puerto Rico. It is a huge bowl-shaped structure lined with reflecting material. The diameter of the bowl is three times as long as a football field. Trees can be seen around the bowl, but they do not shade the bowl significantly.

Diffraction is not only a problem for optical instruments but also for the electromagnetic radiation itself. Any beam of light having a finite diameter $D$ and a wavelength $\lambda$ exhibits diffraction spreading. The beam spreads out with an angle $\theta$ given by the equation $\theta =1.22\frac{\lambda }{D}$ . Take, for example, a laser beam made of rays as parallel as possible (angles between rays as close to $\theta =0º$ as possible) instead spreads out at an angle $\theta =1.22 \lambda /D$ , where $D$ is the diameter of the beam and $\lambda$ is its wavelength. This spreading is impossible to observe for a flashlight, because its beam is not very parallel to start with. However, for long-distance transmission of laser beams or microwave signals, diffraction spreading can be significant ( see [Figure 5]). To avoid this, we can increase $D$ . This is done for laser light sent to the Moon to measure its distance from the Earth. The laser beam is expanded through a telescope to make $D$ much larger and $\theta$ smaller.

The drawing shows a parabolic dish antenna mounted on a scaffolding tower and oriented to the right. The diameter of the dish is D. A horizontal line extends to the right from the top rim of the dish. Above the top line appears another line leaving the rim of the dish and angling up and to the right. The angle between this line and the horizontal line is labeled theta. Analogous lines appear at the bottom rim of the dish, except that the angled line extends down and to the right.

In most biology laboratories, resolution is presented when the use of the microscope is introduced. The ability of a lens to produce sharp images of two closely spaced point objects is called resolution. The smaller the distance $x$

by which two objects can be separated and still be seen as distinct, the greater the resolution. The resolving power of a lens is defined as that distance $x$ . An expression for resolving power is obtained from the Rayleigh criterion. In [Figure 6](a) we have two point objects separated by a distance $x$ . According to the Rayleigh criterion, resolution is possible when the minimum angular separation is

$$\theta =1.22\frac{\lambda }{D}=\frac{x}{d}\text{,} $$

where $d$ is the distance between the specimen and the objective lens, and we have used the small angle approximation (i.e., we have assumed that $x$ is much smaller than $d$ ), so that $\tan \theta \approx \sin \theta \approx \theta$.

Therefore, the resolving power is

$$x=1.22\frac{\lambda d}{D}\text{.} $$

Another way to look at this is by re-examining the concept of Numerical Aperture ( $\text{NA}$ ) discussed in Microscopes. There, $\text{NA}$ is a measure of the maximum acceptance angle at which the fiber will take light and still contain it within the fiber. [Figure 6](b) shows a lens and an object at point P. The $\text{NA}$ here is a measure of the ability of the lens to gather light and resolve fine detail. The angle subtended by the lens at its focus is defined to be $\theta =2\alpha$ . From the figure and again using the small angle approximation, we can write

$$\sin \alpha =\frac{D/2}{d}=\frac{D}{2d}\text{.} $$

The $\text{NA}$ for a lens is $\text{NA}=n \sin \alpha$ , where $n$ is the index of refraction of the medium between the objective lens and the object at point P.

From this definition for $\text{NA}$ , we can see that

$$x=1.22\frac{\lambda d}{D}=1.22\frac{\lambda }{2 \sin \alpha }=0.61\frac{\lambda n}{\text{NA}}\text{.} $$

In a microscope, $\text{NA}$ is important because it relates to the resolving power of a lens. A lens with a large $\text{NA}$ will be able to resolve finer details. Lenses with larger $\text{NA}$ will also be able to collect more light and so give a brighter image. Another way to describe this situation is that the larger the $\text{NA}$ , the larger the cone of light that can be brought into the lens, and so more of the diffraction modes will be collected. Thus the microscope has more information to form a clear image, and so its resolving power will be higher.

Part a of the figure shows two small objects arranged vertically a distance x one above the other on the left side of the schematic. On the right side, at a distance lowercase d from the two objects, is a vertical oval shape that represents a convex lens. The middle of the lens is on the horizontal bisector between the two points on the left. Two rays, one from each object on the left, leave the objects and pass through the center of the lens. The distance d is significantly longer than the distance x. Part b of the figure shows a horizontal oval representing a convex lens labeled microscope objective that is a distance lowercase d above a flat surface. The oval’s long axis is of length capital D. A point P is labeled on the plane directly below the center of the lens, and two rays leave this point. One ray extends to the left edge of the lens and the other ray extends to the right edge of the lens. The angle between these rays is labeled acceptance angle theta, and the half angle is labeled alpha. The distance lowercase d is longer than the distance capital D.

One of the consequences of diffraction is that the focal point of a beam has a finite width and intensity distribution. Consider focusing when only considering geometric optics, shown in [Figure 7](a). The focal point is infinitely small with a huge intensity and the capacity to incinerate most samples irrespective of the $\text{NA}$ of the objective lens. For wave optics, due to diffraction, the focal point spreads to become a focal spot ( see [Figure 7](b)) with the size of the spot decreasing with increasing $\text{NA}$ . Consequently, the intensity in the focal spot increases with increasing $\text{NA}$ . The higher the $\text{NA}$ , the greater the chances of photodegrading the specimen. However, the spot never becomes a true point.

The first schematic is labeled geometric optics focus. It shows an edge-on view of a thin lens that is vertical. The lens is represented by a thin ellipse. Two parallel horizontal rays impinge upon the lens from the left. One ray goes through the upper edge of the lens and is deviated downward at about a thirty degree angle below the horizontal. The other ray goes through the lower edge of the lens and is deviated upward at about a thirty degree angle above the horizontal. These two rays cross a point that is labeled focal point. The second schematic is labeled wave optics focus. It is similar to the first schematic, except that the rays do not quite cross at the focal point. Instead, they diverge away from each other at the same angle as they approached each other. The region of closest approach for the lines is called the focal region.

Section Summary

Conceptual Questions

A beam of light always spreads out. Why can a beam not be created with parallel rays to prevent spreading? Why can lenses, mirrors, or apertures not be used to correct the spreading?

Problems & Exercises

The 300-m-diameter Arecibo radio telescope pictured in [Figure 4] detects radio waves with a 4.00 cm average wavelength.

(a) What is the angle between two just-resolvable point sources for this telescope?

(b) How close together could these point sources be at the 2 million light year distance of the Andromeda galaxy?

Strategy

Use the Rayleigh criterion θ = 1.22λ/D for part (a). For part (b), use s = rθ to find the linear separation at the given distance.

Solution

Given:

(a) Minimum resolvable angle:

$$\theta = 1.22\frac{\lambda}{D} = 1.22\frac{0.0400}{300} = 1.63 \times 10^{-4} \text{ rad}$$

(b) Minimum separation at Andromeda distance:

Convert distance: 1 ly ≈ 9.46 × 10¹⁵ m

$$r = 2 \times 10^6 \text{ ly} \times 9.46 \times 10^{15} \text{ m/ly} = 1.89 \times 10^{22} \text{ m}$$
$$s = r\theta = (1.89 \times 10^{22})(1.63 \times 10^{-4}) = 3.08 \times 10^{18} \text{ m}$$

Converting back to light years:

$$s = \frac{3.08 \times 10^{18}}{9.46 \times 10^{15}} = 326 \text{ ly}$$

Discussion

Despite Arecibo’s enormous 300-m diameter, radio waves have much longer wavelengths than visible light (4 cm vs ~550 nm, a factor of ~70,000 times longer). This gives relatively poor angular resolution (1.63 × 10⁻⁴ rad) compared to optical telescopes. At Andromeda’s distance, the telescope can only resolve features separated by 326 light years—larger than the distance between many nearby stars. This demonstrates why radio astronomy often uses interferometric arrays (like the VLA) to achieve better resolution by effectively increasing D.

Assuming the angular resolution found for the Hubble Telescope in [Example 1], what is the smallest detail that could be observed on the Moon?

Strategy

From Example 1, Hubble’s angular resolution is θ = 2.80 × 10⁻⁷ rad. Use s = rθ with r = distance to Moon ≈ 3.84 × 10⁸ m.

Solution

$$s = r\theta = (3.84 \times 10^8 \text{ m})(2.80 \times 10^{-7} \text{ rad}) = 108 \text{ m}$$

Discussion

Hubble can resolve details as small as 108 m (about the length of a football field) on the Moon. This is why Hubble cannot see the Apollo landing sites - the lunar modules and equipment are only a few meters in size, far below this resolution limit.

Diffraction spreading for a flashlight is insignificant compared with other limitations in its optics, such as spherical aberrations in its mirror. To show this, calculate the minimum angular spreading of a flashlight beam that is originally 5.00 cm in diameter with an average wavelength of 600 nm.

Strategy

Use the Rayleigh criterion θ = 1.22λ/D for the diffraction spreading angle.

Solution

Given:

$$\theta = 1.22\frac{\lambda}{D} = 1.22\frac{600 \times 10^{-9}}{0.0500}$$
$$\theta = \frac{7.32 \times 10^{-7}}{0.0500} = 1.46 \times 10^{-5} \text{ rad}$$

Converting to degrees: θ = 1.46 × 10⁻⁵ rad × (180°/π) = 8.4 × 10⁻⁴ degrees ≈ 0.05 arcminutes

Discussion

This extremely small diffraction angle (0.00146 milliradians or about 3 arcseconds) is indeed negligible compared to other optical imperfections. Typical flashlight beams have divergence angles of several degrees due to:

The diffraction limit would only become important for very high-quality, nearly perfect optical systems. For a flashlight at 100 m distance, diffraction would spread the beam by only s = (100)(1.46 × 10⁻⁵) = 1.5 mm, which is completely insignificant compared to the beam’s actual spread of several meters due to optical imperfections.

(a) What is the minimum angular spread of a 633-nm wavelength He-Ne laser beam that is originally 1.00 mm in diameter?

(b) If this laser is aimed at a mountain cliff 15.0 km away, how big will the illuminated spot be?

(c) How big a spot would be illuminated on the Moon, neglecting atmospheric effects? (This might be done to hit a corner reflector to measure the round-trip time and, hence, distance.) Explicitly show how you follow the steps in Problem-Solving Strategies for Wave Optics.

Strategy

Step 1: This is a diffraction spreading problem. Step 2: Use θ = 1.22λ/D for circular beam diffraction. Step 3: (a) Find θ; (b) find spot size at 15 km; (c) find spot size at Moon distance. Step 4: Given: λ = 633 nm, D = 1.00 mm.

(a) Angular spread:

$$\theta = 1.22\frac{\lambda}{D} = 1.22\frac{633 \times 10^{-9}}{1.00 \times 10^{-3}} = 7.72 \times 10^{-4} \text{ rad}$$

(b) Spot size at 15.0 km:

$$s = r\theta = (15.0 \times 10^3)(7.72 \times 10^{-4}) = 11.6 \text{ m (diameter)}$$

(c) Spot size on Moon (r = 3.84 × 10⁸ m):

$$s = (3.84 \times 10^8)(7.72 \times 10^{-4}) = 2.96 \times 10^5 \text{ m} = 296 \text{ km}$$

Step 5: These results are reasonable - laser beams spread due to diffraction despite being highly collimated.

Discussion

A 296-km spot on the Moon from a 1-mm beam shows significant diffraction spreading. To reduce this, lasers sent to the Moon are expanded through telescopes to increase D, reducing θ = 1.22λ/D.

A telescope can be used to enlarge the diameter of a laser beam and limit diffraction spreading. The laser beam is sent through the telescope in opposite the normal direction and can then be projected onto a satellite or the Moon.

(a) If this is done with the Mount Wilson telescope, producing a 2.54-m-diameter beam of 633-nm light, what is the minimum angular spread of the beam?

(b) Neglecting atmospheric effects, what is the size of the spot this beam would make on the Moon, assuming a lunar distance of $3.84 \times 10^{8} \text{m}$ ?

Strategy

Use θ = 1.22λ/D for part (a), then s = rθ for part (b) to find the spot diameter on the Moon.

Solution

Given:

(a) Minimum angular spread:

$$\theta = 1.22\frac{\lambda}{D} = 1.22\frac{633 \times 10^{-9}}{2.54}$$
$$\theta = \frac{7.72 \times 10^{-7}}{2.54} = 3.04 \times 10^{-7} \text{ rad}$$

(b) Spot size on the Moon:

$$s = r\theta = (3.84 \times 10^8)(3.04 \times 10^{-7}) = 117 \text{ m (radius)}$$

Diameter: 2 × 117 m = 235 m

Discussion

By expanding the laser beam to 2.54 m diameter using the telescope, the diffraction spreading is dramatically reduced compared to the 1-mm beam in the previous problem (which gave a 296-km spot). The spot size on the Moon is now only 235 m in diameter—over 1000 times smaller!

This technique is actually used in lunar laser ranging experiments, where pulses from Earth-based lasers reflect off corner retroreflectors left by Apollo astronauts. The expanded beam reduces diffraction spreading, allowing more photons to hit the small retroreflector targets and return to Earth for precise distance measurements (accurate to a few centimeters).

The limit to the eye’s acuity is actually related to diffraction by the pupil.

(a) What is the angle between two just-resolvable points of light for a 3.00-mm-diameter pupil, assuming an average wavelength of 550 nm?

(b) Take your result to be the practical limit for the eye. What is the greatest possible distance a car can be from you if you can resolve its two headlights, given they are 1.30 m apart?

(c) What is the distance between two just-resolvable points held at an arm’s length (0.800 m) from your eye?

(d) How does your answer to (c) compare to details you normally observe in everyday circumstances?

(a) Minimum resolvable angle:

$$\theta = 1.22\frac{\lambda}{D} = 1.22\frac{550 \times 10^{-9}}{3.00 \times 10^{-3}} = 2.24 \times 10^{-4} \text{ rad}$$

Converting: θ = 2.24 × 10⁻⁴ rad × (180/π) × 60 = 0.77 arcmin ≈ 46 arcseconds

(b) Maximum distance to resolve headlights:

$$r = \frac{s}{\theta} = \frac{1.30}{2.24 \times 10^{-4}} = 5800 \text{ m} = 5.8 \text{ km}$$

(c) Separation at arm’s length:

$$s = r\theta = (0.800)(2.24 \times 10^{-4}) = 1.79 \times 10^{-4} \text{ m} = 0.18 \text{ mm}$$

(d) Comparison: 0.18 mm is about twice the width of a human hair (~0.1 mm) and matches our everyday experience - we can barely distinguish two dots separated by this distance at arm’s length. This is consistent with typical human visual acuity of about 20/20 vision.

What is the minimum diameter mirror on a telescope that would allow you to see details as small as 5.00 km on the Moon some 384 000 km away? Assume an average wavelength of 550 nm for the light received.

Strategy

Use s = rθ to find the required angular resolution, then use θ = 1.22λ/D to solve for the minimum diameter D.

Solution

Given:

Step 1: Find required angular resolution

$$\theta = \frac{s}{r} = \frac{5000}{3.84 \times 10^8} = 1.302 \times 10^{-5} \text{ rad}$$

Step 2: Find minimum mirror diameter

Using θ = 1.22λ/D:

$$D = \frac{1.22\lambda}{\theta} = \frac{1.22 \times 550 \times 10^{-9}}{1.302 \times 10^{-5}}$$
$$D = \frac{6.71 \times 10^{-7}}{1.302 \times 10^{-5}} = 0.0515 \text{ m} = 5.15 \text{ cm}$$

Discussion

A surprisingly small telescope mirror of only 5.15 cm (about 2 inches) diameter is theoretically sufficient to resolve 5-km features on the Moon—assuming perfect optics and no atmospheric distortion. This is within the range of good amateur telescopes.

However, in practice, atmospheric turbulence (seeing) limits ground-based telescopes to resolution of about 1 arcsecond (roughly 2 km on the Moon), regardless of aperture size. This is why even large telescopes on Earth can’t significantly outperform small ones for lunar observations unless adaptive optics is used to compensate for atmospheric effects. Space-based telescopes like Hubble avoid this problem entirely.

You are told not to shoot until you see the whites of their eyes. If the eyes are separated by 6.5 cm and the diameter of your pupil is 5.0 mm, at what distance can you resolve the two eyes using light of wavelength 555 nm?

Strategy

Find the minimum resolvable angle θ = 1.22λ/D, then find the maximum distance r = s/θ where the eyes can be resolved.

Solution

$$\theta = 1.22\frac{\lambda}{D} = 1.22\frac{555 \times 10^{-9}}{5.0 \times 10^{-3}} = 1.35 \times 10^{-4} \text{ rad}$$
$$r = \frac{s}{\theta} = \frac{0.065}{1.35 \times 10^{-4}} = 481 \text{ m}$$

Discussion

You could resolve the two eyes at distances up to about 480 m. This is remarkably far - nearly half a kilometer! Of course, in practice, other factors like atmospheric turbulence and the need to see details smaller than eye separation would limit the actual distance.

(a) The planet Pluto and its Moon Charon are separated by 19 600 km. Neglecting atmospheric effects, should the 5.08-m-diameter Mount Palomar telescope be able to resolve these bodies when they are $4.50 \times 10^{9} \text{km}$ from Earth? Assume an average wavelength of 550 nm.

(b) In actuality, it is just barely possible to discern that Pluto and Charon are separate bodies using an Earth-based telescope. What are the reasons for this?

Strategy

For part (a), calculate the angular separation of Pluto and Charon, then compare to the telescope’s angular resolution θ = 1.22λ/D. For part (b), consider atmospheric effects.

Solution

Given:

(a) Can the telescope resolve Pluto and Charon?

Angular separation:

$$\theta_{\text{sep}} = \frac{s}{r} = \frac{1.96 \times 10^7}{4.50 \times 10^{12}} = 4.36 \times 10^{-6} \text{ rad}$$

Telescope’s angular resolution (diffraction limit):

$$\theta_{\text{min}} = 1.22\frac{\lambda}{D} = 1.22\frac{550 \times 10^{-9}}{5.08} = 1.32 \times 10^{-7} \text{ rad}$$

Comparison:

$$\frac{\theta_{\text{sep}}}{\theta_{\text{min}}} = \frac{4.36 \times 10^{-6}}{1.32 \times 10^{-7}} = 33$$

Since the angular separation is 33 times larger than the diffraction limit, yes, the telescope should easily resolve Pluto and Charon (neglecting atmospheric effects).

(b) Why is it just barely possible in reality?

The fact that it’s just barely possible (rather than easy) to distinguish Pluto and Charon indicates severe atmospheric aberrations:

  1. Atmospheric turbulence (seeing) limits ground-based telescopes to angular resolution of about 0.5-1.0 arcsecond (2.4-4.8 × 10⁻⁶ rad) under good conditions—comparable to the 4.36 × 10⁻⁶ rad separation
  2. Atmospheric refraction causes image distortion and blurring
  3. Thermal air currents create “twinkling” that smears the images
  4. Limited integration time means astronomers can’t always capture moments of best seeing

The diffraction limit (1.32 × 10⁻⁷ rad) is 30-60 times better than atmospheric seeing limits. This is why space-based telescopes like Hubble can achieve their full diffraction-limited performance, while even the largest ground-based telescopes are limited by the atmosphere unless adaptive optics is used.

Discussion

This problem dramatically illustrates how Earth’s atmosphere, not optics, limits most ground-based astronomical observations. A perfect 5-meter telescope in space would easily resolve Pluto-Charon, but from Earth’s surface, atmospheric turbulence reduces the effective resolution by a factor of 30 or more, making the observation just barely possible.

The headlights of a car are 1.3 m apart. What is the maximum distance at which the eye can resolve these two headlights? Take the pupil diameter to be 0.40 cm.

Strategy

Use θ = 1.22λ/D with λ ≈ 550 nm, D = 0.40 cm = 4.0 mm, then r = s/θ.

Solution

$$\theta = 1.22\frac{550 \times 10^{-9}}{4.0 \times 10^{-3}} = 1.68 \times 10^{-4} \text{ rad}$$
$$r = \frac{s}{\theta} = \frac{1.3}{1.68 \times 10^{-4}} = 7740 \text{ m} \approx 7.7 \text{ km}$$

Discussion

The maximum distance is about 7.7 km. At night with dilated pupils (larger D), this distance would be somewhat shorter. In practice, atmospheric effects, haze, and the need to see the headlights’ size (not just their separation) reduce the effective distance.

When dots are placed on a page from a laser printer, they must be close enough so that you do not see the individual dots of ink. To do this, the separation of the dots must be less than Raleigh’s criterion. Take the pupil of the eye to be 3.0 mm and the distance from the paper to the eye of 35 cm; find the minimum separation of two dots such that they cannot be resolved. How many dots per inch (dpi) does this correspond to?

Strategy

Find θ = 1.22λ/D, then minimum separation s = rθ at distance r = 35 cm. Convert to dpi.

Solution

$$\theta = 1.22\frac{550 \times 10^{-9}}{3.0 \times 10^{-3}} = 2.24 \times 10^{-4} \text{ rad}$$
$$s = r\theta = (0.35)(2.24 \times 10^{-4}) = 7.84 \times 10^{-5} \text{ m} = 78.4 \text{ μm}$$

Dots per inch:

$$\text{dpi} = \frac{1 \text{ inch}}{s} = \frac{0.0254 \text{ m}}{7.84 \times 10^{-5} \text{ m}} = 324 \text{ dpi}$$

Discussion

A resolution of about 300-324 dpi is sufficient to make individual dots unresolvable at normal reading distance (35 cm). This is why 300 dpi became the standard for laser printers - it exceeds the eye’s diffraction-limited resolution. Higher dpi (600, 1200) improves quality for closer viewing or finer details but isn’t necessary for normal reading.

Unreasonable Results

An amateur astronomer wants to build a telescope with a diffraction limit that will allow him to see if there are people on the moons of Jupiter.

(a) What diameter mirror is needed to be able to see 1.00 m detail on a Jovian Moon at a distance of $7.50 \times 10^{8} \text{km}$ from Earth? The wavelength of light averages 600 nm.

(b) What is unreasonable about this result?

(c) Which assumptions are unreasonable or inconsistent?

Strategy

Use Rayleigh criterion θ = 1.22λ/D and s = rθ to find required D.

Solution

(a) Required mirror diameter:

Given: s = 1.00 m, r = 7.50 × 10⁸ km = 7.50 × 10¹¹ m, λ = 600 nm

$$\theta = \frac{s}{r} = \frac{1.00}{7.50 \times 10^{11}} = 1.33 \times 10^{-12} \text{ rad}$$

Using θ = 1.22λ/D:

$$D = \frac{1.22\lambda}{\theta} = \frac{1.22 \times 600 \times 10^{-9}}{1.33 \times 10^{-12}} = 5.50 \times 10^5 \text{ m} = 550 \text{ km}$$

(b) What is unreasonable?

A mirror diameter of 550 km is absurdly large:

(c) Unreasonable assumptions:

  1. Expecting to resolve 1-m details at Jupiter’s distance (750 million km) is unrealistic for any ground or even space-based telescope
  2. The diffraction limit makes such resolution physically impossible without an impossibly large aperture
  3. Even if built, atmospheric turbulence would prevent this resolution from Earth
  4. The assumption that an “amateur” could build such a telescope is absurd

Discussion

This illustrates why we can’t see fine details on distant planets. Even Hubble (2.4 m) can only resolve features ~150 km on Jupiter. To see people (meter-scale) would require space-based interferometry with baseline separations of hundreds of kilometers, far beyond amateur (or even professional single-telescope) capabilities.

Construct Your Own Problem

Consider diffraction limits for an electromagnetic wave interacting with a circular object. Construct a problem in which you calculate the limit of angular resolution with a device, using this circular object (such as a lens, mirror, or antenna) to make observations. Also calculate the limit to spatial resolution ( such as the size of features observable on the Moon) for observations at a specific distance from the device. Among the things to be considered are the wavelength of electromagnetic radiation used, the size of the circular object, and the distance to the system or phenomenon being observed.

Glossary

Rayleigh criterion
two images are just resolvable when the center of the diffraction pattern of one is directly over the first minimum of the diffraction pattern of the other