Design a Telescope Optics for Spy Satellite- Angular Resolution & Mirror Size

In summary: Not very feasible.In summary, the conversation discusses designing a telescope for a spy satellite that can clearly see objects as small as 1 inch from a distance of 500 km above Earth's surface. The angular resolution and size of the primary mirror are calculated, with the feasibility of the design being questioned due to the size and launch requirements.
  • #1
BurnieMac
3
0

Homework Statement


This is a question on my final review.

Imagine you are given the task of designing the telescope in a spy satellite that is
going to be launched into an orbit 500 km above the surface of the Earth. The agency you
are working for wants to be able to clearly see objects as small as 1 inch = 2.5 cm (for
example the headlines on a newspaper).

a.) Calculate the angular resolution needed to achieve this.

b.) Given that diffraction is the ultimate limitation of your telescope, how big will the
primary mirror need to be? Use 500 nm for the wavelength of the light.

c) In one or two sentences, comment on the feasibility of your design. Hint: for
comparison the largest Earth based telescope has a 10 meter diameter mirror, the Hubble
space telescope has a 2.4 meter diameter mirror.

--

I am really lost.. My knowledge is very poor for this chapter, I read the chapter earlier and still don't know.

Much help from your bright minds would be appreciated!


Homework Equations




Not sure

The Attempt at a Solution


a. )
Theta = Object height / Object Distance
In that case it is 5.0x10^-8 degrees
b.) How big will the mirror have to be..
I used rayleigh's criterion.
Theta(min) = 1.22(wavelength) / D
Solved for D, giving 12.2m
c.) No idea
 
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  • #2
BurnieMac said:

The Attempt at a Solution


a. )
Theta = Object height / Object Distance
In that case it is 5.0x10^-8 degrees
b.) How big will the mirror have to be..
I used rayleigh's criterion.
Theta(min) = 1.22(wavelength) / D
Solved for D, giving 12.2m
c.) No idea
(a) Okay, but that should be in radians.
(b) Looks good.
(c) Mainly a common-sense question. How feasible is it to launch a telescope 5x larger (and 25x times the area) of Hubble? Or to not only build something larger than any telescope that has ever been built, ever, but launch it into orbit as well?
 

1. How does the angular resolution of a telescope affect its ability to spy on objects?

The angular resolution of a telescope determines its ability to distinguish fine details and resolve objects that are close together. This is especially important for spy satellites as it allows them to capture clear and detailed images of objects on the ground.

2. What factors affect the angular resolution of a telescope?

The angular resolution of a telescope is affected by two main factors: the diameter of the primary mirror and the wavelength of light being observed. A larger primary mirror allows for better resolution, while shorter wavelengths of light provide sharper images.

3. How do you determine the appropriate mirror size for a spy satellite telescope?

The appropriate mirror size for a spy satellite telescope is determined by the desired angular resolution and the wavelength of light being observed. The formula for calculating the minimum diameter of the primary mirror is D = 1.22 * λ / θ, where D is the diameter of the mirror, λ is the wavelength, and θ is the desired angular resolution.

4. Can a telescope's angular resolution be improved without increasing the size of the primary mirror?

Yes, there are other techniques that can be used to improve the angular resolution of a telescope, such as adaptive optics and interferometry. These methods use advanced technologies to correct for atmospheric distortions and combine the light from multiple telescopes, respectively.

5. Are there any limitations to the size of a spy satellite telescope's mirror?

Yes, there are limitations to the size of a spy satellite telescope's mirror due to the constraints of launching and operating in space. The mirror must be compact and lightweight, and the satellite must be able to withstand the forces of launch and extreme temperatures in orbit.

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