courses:ast201:7
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courses:ast201:7 [2023/08/20 01:35] – [2.5 Schmidt telescopes] asad | courses:ast201:7 [2023/11/26 00:02] (current) – [3.3 Pros and cons] asad | ||
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The corrector plate then removes SA. The marginal rays ($\rho$ large) converge more strongly than the axial rays ($\rho$ small, closer to axis) as you saw in Section 5.3 of Chapter 6. A Schmidt corrector has higher power for the axial rays than for the marginals, this bringing all rays to a common focal plane. | The corrector plate then removes SA. The marginal rays ($\rho$ large) converge more strongly than the axial rays ($\rho$ small, closer to axis) as you saw in Section 5.3 of Chapter 6. A Schmidt corrector has higher power for the axial rays than for the marginals, this bringing all rays to a common focal plane. | ||
+ | |||
===== - Space telescopes ===== | ===== - Space telescopes ===== | ||
+ | |||
+ | ==== - Resolution ==== | ||
+ | $$ \theta = 2\alpha = \frac{2.44 \lambda}{D} $$ | ||
+ | |||
+ | ==== - Sensitivity ==== | ||
+ | |||
+ | The number of photons detected by a detector is the **Signal** | ||
+ | |||
+ | $$ S = \frac{\pi D^2}{4} \frac{\lambda}{hc} f_\lambda tQ $$ | ||
+ | |||
+ | where the factor $hc/ | ||
+ | |||
+ | A star is detectable if $S$ is about the same size as its uncertainty. The measurement | ||
+ | |||
+ | $$ M = S+B $$ | ||
+ | |||
+ | where $B$ is the **background** containing everything other than the star in the image. The background can actually be both in front of the star or behind star or at the same distance as the star. The background | ||
+ | |||
+ | $$ B = \frac{\pi D^2}{4} \frac{\lambda}{hc} \frac{\pi\theta^2}{4} b_\lambda tQ $$ | ||
+ | |||
+ | where $\theta$ is the size of the star in the image and $b_\lambda$ the actual background flux. Now according to Poisson statistics the uncertainty in counting photons, the noise, | ||
+ | |||
+ | $$ N = \sigma(S) = \sqrt{(S+B)+B} \approx \sqrt{2B} = \frac{\pi D\theta}{4} \left(\frac{2\lambda b_\lambda tQ}{hc}\right)^{1/ | ||
+ | |||
+ | and, thereby, the signal-to-noise-ratio (SNR) | ||
+ | |||
+ | $$ \frac{S}{N} \approx \left(\frac{\lambda Qt}{hcb_\lambda}\right) \frac{D}{\theta} f_\lambda $$ | ||
+ | |||
+ | for a star that is marginally detectable. Purring $S/N=1$ results in the flux of such a star | ||
+ | |||
+ | $$ f_\lambda = \sqrt{\frac{hc}{\lambda Q}} \sqrt{\frac{b_\lambda}{t}} \frac{\theta}{D} $$ | ||
+ | |||
+ | for a telescope whose image results in the diameter of a star to be $\theta$. In case of ground-based telescope, the size is that of the **seeing disk**. For space telescope putting $\theta=2.44\lambda / D$ gives | ||
+ | |||
+ | $$ f_{d,space} = \sqrt{\frac{hc\lambda}{Q}} \sqrt{\frac{b_\lambda}{t}} \frac{2.44}{D^2} $$ | ||
+ | |||
+ | which means, increasing the aperture size gives a huge advantage in case of space telescopes because $f_d \propto D^{-2}$ in that case. | ||
+ | |||
+ | ==== - Pros and cons ==== | ||
+ | Advantages are as follows. | ||
+ | |||
+ | - Background $b_\lambda$: | ||
+ | - Atmospheric transmission | ||
+ | - Visible sky area | ||
+ | - Gravitational and frictional stress | ||
+ | |||
+ | Disadvantages are as follows. | ||
+ | |||
+ | - Cost. One 8-m Gemini telescope cost 100 million USD, and one 2.4-m HST telescope cost 2 billion USD. | ||
+ | - Thermal stress | ||
+ | - Harmful radiation, high-energy particles | ||
===== - Ground-based telescopes ===== | ===== - Ground-based telescopes ===== | ||
+ | The [[wp> | ||
+ | |||
+ | - Casting: molten glass poured into a cylindrical mold | ||
+ | - Annealing | ||
+ | - Grinding and polishing | ||
+ | {{: | ||
===== - Adaptive optics ===== | ===== - Adaptive optics ===== | ||
courses/ast201/7.1692516935.txt.gz · Last modified: by asad