courses:ast201:7
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courses:ast201:7 [2023/08/20 00:49] – [2.2 Cassegrain and Georgian] asad | courses:ast201:7 [2023/11/26 00:02] (current) – [3.3 Pros and cons] asad | ||
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The tube of the Cassegrain is much shorter than a Newtonian which means Cassegrain is much cheaper to build. A Gregorian is longer than a Cassegrain but still shorter than a Newtonian. | The tube of the Cassegrain is much shorter than a Newtonian which means Cassegrain is much cheaper to build. A Gregorian is longer than a Cassegrain but still shorter than a Newtonian. | ||
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+ | The conic constant for the primary $K_1=-1$ (paraboloid) for both, and for Cassegrain the conic constant for the secondary | ||
+ | |||
+ | $$ K_2 = -\left(\frac{m+1}{m-1}\right)^2 $$ | ||
+ | |||
+ | which is determined by the requirement that SA should be zero. | ||
+ | |||
+ | ==== - Ritchey–Chrétien (RC) ==== | ||
+ | Both Gregorian and Cassegrain have $K=-1$ which means they cannot avoid coma and astigmatism. But an **aplanatic** (without coma and astigmatism) two-mirror telescope called the Ritchey–Chrétien (RC) is made using a primary mirror of different. In an RC, both the primary and secondary are hyperboloid and their conic constants | ||
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+ | $$ K_1 = K_{1c} - \frac{2(1+\beta)}{m^2(m-\beta)} $$ | ||
+ | |||
+ | $$ K_2 = K_{2c} - \frac{2m(m+1)}{(m-\beta)(m-1)^3} $$ | ||
+ | |||
+ | where $K_{1c}$ and $K_{2c}$ are the conis constants of the Cassegrain. | ||
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+ | RC reduces coma and astigmatism, | ||
+ | |||
+ | ==== - Nasmyth and coudé foci ==== | ||
+ | Below panel (a) shows the Nasmyth focus and (b) the coudé focus. Both are used in cases when heavier instruments need to be placed at the final focus. Nasmyth can take heavier instruments than Cassegrain and RC, but coudé can take even more load than Nasmyth. | ||
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+ | {{: | ||
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+ | In (a) a flat mirror intercepts the light from the secondary and redirects it horizontally along the altitude axis to the Nasmyth focus which remains fixed relative to the mount during tracking. Gravitational stress on the telescope and mount do not change over time for this. | ||
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+ | In (b) (shown in an equatorial mount here) the light from the secondary is intercepted and, first, brought along the declination axis and then to the polar axis. | ||
+ | |||
+ | ==== - Schmidt telescopes ==== | ||
+ | RC can give good quality images for up to 1 deg, and maybe up to 3 deg with corrector lenses. Schmidt telescopes are used for larger field of view, 6 to 8 deg. They are specially good for photographic surveys. | ||
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+ | {{: | ||
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+ | In this configuration, | ||
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+ | Light from different angles illuminate different parts of the primary, and the focal surface, but the chief ray from any direction always passes through $C$. So $b=0$ and all off-axis aberrations are gone. | ||
+ | |||
+ | 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/ | ||
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+ | 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, | ||
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+ | $$ N = \sigma(S) = \sqrt{(S+B)+B} \approx \sqrt{2B} = \frac{\pi D\theta}{4} \left(\frac{2\lambda b_\lambda tQ}{hc}\right)^{1/ | ||
+ | |||
+ | and, thereby, the signal-to-noise-ratio (SNR) | ||
+ | |||
+ | $$ \frac{S}{N} \approx \left(\frac{\lambda Qt}{hcb_\lambda}\right) \frac{D}{\theta} f_\lambda $$ | ||
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+ | for a star that is marginally detectable. Purring $S/N=1$ results in the flux of such a star | ||
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+ | $$ f_\lambda = \sqrt{\frac{hc}{\lambda Q}} \sqrt{\frac{b_\lambda}{t}} \frac{\theta}{D} $$ | ||
+ | |||
+ | for a telescope whose image results in the diameter of a star to be $\theta$. In case of ground-based telescope, the size is that of the **seeing disk**. For space telescope putting $\theta=2.44\lambda / D$ gives | ||
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+ | $$ 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 ===== | ||
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