BAAO 2017, Теория — Задача 5. Imaging an Exoplanet

British Astronomy and Astrophysics Olympiad 2016-2017 — Astronomy & Astrophysics Competition Paper — Monday 23rd January 2017 · 23 януари 2017 г. · 20 т.

Указания

Time: 3 hours plus 15 minutes reading time (no writing permitted). Approx 35 minutes per question.

Questions: All five questions should be attempted.

Marks: The questions carry similar marks.

Solutions: Answers and calculations are to be written on loose paper or in examination booklets. Students should ensure their name and school is clearly written on all answer sheets and pages are numbered. A standard formula booklet with standard physical constants should be supplied.

Instructions: To accommodate students sitting the paper at different times, please do not discuss any aspect of the paper on the internet until 8 am Saturday 28th January.

Clarity: Solutions must be written legibly, in black pen (the papers are photocopied), and working down the page. Scribble will not be marked and overall clarity is an important aspect of this exam paper.

Eligibility: The International Olympiad will be held during November 2017; all sixth form students are eligible to participate, even if they will be attending university in November.

Training Dates and the International Astronomy and Astrophysics Olympiad (IOAA)

The IOAA this year will be held in Phuket, Thailand, from 12th to 21st November 2017.

The team will be selected from sixth form students taking this paper and Y12 students taking the AS Challenge in March. The best students eligible to represent the UK at the IOAA will be invited to attend the Training Camp to be held in the Physics Department at the University of Oxford, (Tuesday 4th April to Friday 7th April 2017). Astronomy material will be covered; problem solving skills and observational skills (telescope and naked eye observations) will be developed. At the Training Camp a data analysis exam and a short theory paper will be sat. Five students (plus one reserve) will be selected for further training. From May there will be mentoring by email to cover some topics and problems, followed by a training camp in the summer and also one in the autumn.

Important Constants
ConstantSymbolValue
Speed of lightcc3.00×108 m s−13.00\times10^{8}\ \mathrm{m\,s^{-1}}
Earth’s rotation period1 day24 hours
Earth’s orbital period1 year365.25 days
parsecpc3.09×1016 m3.09\times10^{16}\ \mathrm{m}
Astronomical UnitAU1.49×1011 m1.49\times10^{11}\ \mathrm{m}
Radius of the EarthR⊕\mathrm{R}_{\oplus}6.37×106 m6.37\times10^{6}\ \mathrm{m}
Semi-major axis of the Earth’s orbit1 AU
Radius of the SunR⊙\mathrm{R}_{\odot}6.96×108 m6.96\times10^{8}\ \mathrm{m}
Mass of the SunM⊙\mathrm{M}_{\odot}1.99×1030 kg1.99\times10^{30}\ \mathrm{kg}
Mass of the EarthM⊕\mathrm{M}_{\oplus}5.97×1024 kg5.97\times10^{24}\ \mathrm{kg}
Luminosity of the SunL⊙\mathrm{L}_{\odot}3.85×1026 W3.85\times10^{26}\ \mathrm{W}
Gravitational constantGG6.67×10−11 m3 kg−1 s−26.67\times10^{-11}\ \mathrm{m^{3}\,kg^{-1}\,s^{-2}}

You might find the diagram of an elliptical orbit below useful in solving some of the questions:

Elements of an elliptic orbit:

a=OA (=OP)a = \mathbf{OA}\ (= \mathbf{OP}) semi-major axis

a=OB (=OC)a = \mathbf{OB}\ (= \mathbf{OC}) semi-minor axis

e=1−b2a2e = \sqrt{1-\frac{b^2}{a^2}} eccentricity

F focus

P periapsis (point nearest to F)

A apoapsis (point furthest from F)

Keplers Third Law: For an elliptical orbit, the square of the period, TT, of orbit of an object about the focus is proportional to the cube of the semi-major axis, aa (the average of the minimum and maximum distances from the Sun). The constant of proportionality is 4π2/GM4\pi^2/GM, where MM is the mass of the central object and GG is the universal gravitational constant.

Magnitudes: The apparent magnitudes of two objects, m1m_1 and m0m_0, are related to their apparent brightnesses, b1b_1 and b0b_0, via the formula:

b1b0=10−0.4(m1−m0)\frac{b_1}{b_0} = 10^{-0.4(m_1-m_0)}
Note for markers

BAAO 2016/17 Solutions and Marking Guidelines

Note for markers:

  • Answers to two or three significant figures are generally acceptable. The solution may give more in order to make the calculation clear.
  • There are multiple ways to solve some of the questions; please accept all good solutions that arrive at the correct answer. If a candidate gets the final (numerical) answer then allow them all the marks for that part of the question (as indicated in red), so long as there are no unphysical / nonsensical steps or assumptions made.

Условие

Recently a group of researchers announced that they had discovered an Earth-sized exoplanet around our nearest star, Proxima Centauri. Its closeness raises an intriguing possibility about whether or not we might be able to image it directly using telescopes. The difficulty comes from the small angular scales that need to be resolved and the extreme differences in brightness between the reflected light from the planet and the light given out by the star.

Artist’s impression: a rocky, rugged landscape in the foreground under a reddish sky, with a small bright star low above the horizon.
Figure 6: Artist’s impression of the view from the surface of Proxima Centauri b. Credit: ESO / M. Kornmesser

Data about the star and the planet are summarised below:

Proxima Centauri (star)Proxima Centauri b (planet)
Distance1.295 pcOrbital period11.186 days
Mass0.123 M⊙0.123\ \mathrm{M}_{\odot}Mass (min)≈1.27 M⊕\approx 1.27\ \mathrm{M}_{\oplus}
Radius0.141 R⊙0.141\ \mathrm{R}_{\odot}Radius (min)≈1.1 R⊕\approx 1.1\ \mathrm{R}_{\oplus}
Surface temperature3042 K
Apparent magnitude11.13

The following formulae may also be helpful:

m−M=5log⁡(d10)M−M⊙=−2.5log⁡(LL⊙)Δm=2.5log⁡CRm - \mathcal{M} = 5\log\left(\frac{d}{10}\right) \qquad \mathcal{M} - \mathcal{M}_{\odot} = -2.5\log\left(\frac{L}{\mathrm{L}_{\odot}}\right) \qquad \Delta m = 2.5\log CR

where mm is the apparent magnitude, M\mathcal{M} is the absolute magnitude, dd is the distance in parsecs, and the contrast ratio (CRCR) is defined as the ratio of fluxes from the star and planet, CR=fstarfplanetCR = \frac{f_{\mathrm{star}}}{f_{\mathrm{planet}}}.

a. Calculate the maximum angular separation between the star and the planet, assuming a circular orbit. Give your answer in arcseconds (3600 arcseconds = 1∘1^{\circ}). [3 т.]

b. Determine the luminosity of the star and hence calculate the flux received on the Earth (in W m−2\mathrm{W\ m^{-2}}) from both the star and the planet. Use them to work out the contrast ratio and thus the apparent magnitude of the planet. Assume the planet reflects half of the incident light and that M⊙=4.83\mathcal{M}_{\odot} = 4.83. [8 т.]

The resolving power of a diffraction limited telescope is given by

θmin⁡=1.22λD\theta_{\min} = 1.22\frac{\lambda}{D}

where λ\lambda is the wavelength being observed at, DD is the diameter of the telescope aperture, and θmin⁡\theta_{\min} is the smallest angular separation (in radians) the telescope can distinguish.

Data about some current and planned telescopes are summarised below:

TelescopeDiameter (m)Faintest mm detectable
Hubble Space Telescope (HST)2.431
Keck II (based in Hawaii)10.0(variable)
James Webb Space Telescope (JWST)6.534

c. Verify that the HST (which is diffraction limited since it’s in space) would be sensitive enough to image the planet in the visible, but is unable to resolve it from its host star (take λ=550\lambda = 550 nm). [2 т.]

Ground-based telescopes have bigger mirrors than the HST, but are not diffraction limited due to movements in the atmosphere and so need to be fitted with ‘adaptive optics’ (AO) to compensate for this effect. However, even with perfect AO the faintest object the telescope can detect is limited by the brightness of the atmosphere.

The signal-to-noise ratio (SNRSNR) can be approximated as:

SNR≈fAϵtfAϵt+bϵtSNR \approx \frac{fA\epsilon t}{\sqrt{fA\epsilon t + b\epsilon t}}

where ff is the flux from the object (in photons m−2 s−1\mathrm{m^{-2}\ s^{-1}}), AA is the area of the telescope mirror, ϵ\epsilon is the overall efficiency of the telescope and detector, bb is the flux from the sky (in photons s−1\mathrm{s^{-1}}), and tt is the length of the exposure.

d. Calculate the exposure time needed for a Keck II image of the exoplanet to have an SNRSNR of 3 (i.e. barely detectable). Assume that the telescope has perfect AO (so it is diffraction limited), is observed at the longest wavelength for which the planet can still be resolved from the star, all the received flux from the planet consists of photons of that longest wavelength, ϵ=0.1\epsilon = 0.1 and b=109b = 10^9 photons s−1\mathrm{s^{-1}} (so b≫fb \gg f). Comment on your answer. [4 т.]

The James Webb Space Telescope (JWST) is the successor to the HST and is due to launch in 2018. It should be able to both resolve the system and cope with the contrast ratio. Since it is in space it is diffraction limited, and the SNRSNR should be dominated by the flux from the planet (i.e. f≫bf \gg b).

e. How long an exposure would JWST need in order to get the same SNRSNR as Keck II, again if observed at the longest wavelength for which the planet can still be resolved from the star by the telescope? (Make similar assumptions about the received flux and use the same value of ϵ\epsilon.) [3 т.]

Отговори

Решение

Questions proposed by

END OF PAPER

Questions proposed by:

Dr Alex Calverley (Bedford School)

Dr Emile Doran (The Langley Academy)

Sandor Kruk (University of Oxford)


Оригинал в Архива: BAAO_2017.pdf · официални решения: BAAO_2017_solutions.pdf