BAAO 2025, II кръг — Задача 3. Gravitational Microlensing

British Astronomy and Astrophysics Olympiad 2024-2025 — Astro Round 2 — Tuesday 25th February 2025 · 25 февруари 2025 г. · 40 т.

Указания

This question paper must not be photographed or taken out of the exam room

Time: 3 hours (∼50\sim 50 minutes for Q1, ∼65\sim 65 minutes for Q2 and ∼65\sim 65 minutes for Q3).

Questions: All three questions should be attempted. Each question contains independent parts so that later parts can be attempted even if earlier parts are incomplete. The questions build in difficulty.

Solutions: Answers and calculations are to be written on loose paper. Students should ensure their name and school is clearly written on the first answer sheet and that all pages are numbered. A standard formula booklet may be used. START EACH QUESTION ON A NEW PAGE.

Clarity: Solutions must be written legibly, in black or blue pen, and working down the page. Scribble will not be marked and overall clarity is an important aspect of this exam.

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 Thursday 6th March.

Calculators: Any standard calculator may be used, but calculators cannot be programmable and must not have symbolic algebra capability.

Training Dates and the IOAA

Training Dates and the IOAA (Mumbai, India, 11th - 21st August 2025)

The best students taking this paper eligible to represent the UK at the IOAA will be invited to attend the Selection Camp to be held in Oxford from Monday 7th to Friday 11th April 2025. At the camp, problem solving skills and observational skills (including with telescopes) will be developed, and students will sit a Data Analysis exam along with the Round 3 paper. From this, a team of five students (plus one reserve) will be selected for further training, including additional camps in the summer.

The BAAO are very proud to be sponsored by G-Research

Important Constants
ConstantSymbolValue
Speed of lightcc3.00×108 m s−13.00 \times 10^{8}\ \mathrm{m\ s^{-1}}
Earth’s rotation period1 day24 hours
Earth’s orbital period1 year365.25 days
parsecpc3.09×1016 m3.09 \times 10^{16}\ \mathrm{m}
Astronomical Unitau1.50×1011 m1.50 \times 10^{11}\ \mathrm{m}
Radius of the SunR⊙R_{\odot}6.96×108 m6.96 \times 10^{8}\ \mathrm{m}
Radius of the EarthR⊕R_{\oplus}6.37×106 m6.37 \times 10^{6}\ \mathrm{m}
Mass of the SunM⊙M_{\odot}1.99×1030 kg1.99 \times 10^{30}\ \mathrm{kg}
Mass of the EarthM⊕M_{\oplus}5.97×1024 kg5.97 \times 10^{24}\ \mathrm{kg}
Luminosity of the SunL⊕L_{\oplus}3.83×1026 W3.83 \times 10^{26}\ \mathrm{W}
Absolute magnitude of the SunM⊙\mathcal{M}_{\odot}4.744.74
Hubble constantH0H_070 km s−1 Mpc−170\ \mathrm{km\ s^{-1}\ Mpc^{-1}}
Stephan-Boltzmann constantσ\sigma5.67×10−8 W m−2 K−45.67 \times 10^{-8}\ \mathrm{W\ m^{-2}\ K^{-4}}
Gravitational constantGG6.67×10−11 m3 kg−1 s−26.67 \times 10^{-11}\ \mathrm{m^{3}\ kg^{-1}\ s^{-2}}
Boltzmann constantkBk_{\mathrm{B}}1.38×10−23 J K−11.38 \times 10^{-23}\ \mathrm{J\ K^{-1}}
Permittivity of free spaceε0\varepsilon_08.85×10−12 F m−18.85 \times 10^{-12}\ \mathrm{F\ m^{-1}}
Permeability of free spaceμ0\mu_04π×10−7 H m−14\pi \times 10^{-7}\ \mathrm{H\ m^{-1}}
Planck’s constanthh6.63×10−34 J s6.63 \times 10^{-34}\ \mathrm{J\ s}
Elementary chargeee1.60×10−19 C1.60 \times 10^{-19}\ \mathrm{C}
Proton rest massmpm_{\mathrm{p}}1.67×10−27 kg1.67 \times 10^{-27}\ \mathrm{kg}
Electron rest massmem_{\mathrm{e}}9.11×10−31 kg9.11 \times 10^{-31}\ \mathrm{kg}
Wien’s displacement lawλmax⁡T\lambda_{\max}T2.90×10−3 m K2.90 \times 10^{-3}\ \mathrm{m\ K}
Avagadro’s constantNAN_A6.02×1023 mol−16.02 \times 10^{23}\ \mathrm{mol^{-1}}

Basic calculus formulae:

Chain rule

ddxf(g(x))=f′(g(x))g′(x)\frac{\mathrm{d}}{\mathrm{d}x}f(g(x)) = f'(g(x))g'(x)

Product rule

ddx(uv)=dudxv+udvdx\frac{\mathrm{d}}{\mathrm{d}x}(uv) = \frac{\mathrm{d}u}{\mathrm{d}x}v + u\frac{\mathrm{d}v}{\mathrm{d}x}

Quotient rule

ddx(uv)=dudxv−udvdxv2\frac{\mathrm{d}}{\mathrm{d}x}\left(\frac{u}{v}\right) = \frac{\frac{\mathrm{d}u}{\mathrm{d}x}v - u\frac{\mathrm{d}v}{\mathrm{d}x}}{v^2}

Integration by parts

∫udvdx dx=uv−∫vdudx dx\int u\frac{\mathrm{d}v}{\mathrm{d}x}\,\mathrm{d}x = uv - \int v\frac{\mathrm{d}u}{\mathrm{d}x}\,\mathrm{d}x

Standard integral

∫1x dx=ln⁡∣x∣+C\int \frac{1}{x}\,\mathrm{d}x = \ln|x| + C
Important Formulae

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
  • b=OB (=OC)b = \mathbf{OB}\ (= \mathbf{OC}) semi-minor axis
  • e=1−b2a2e = \sqrt{1 - \frac{b^2}{a^2}} eccentricity
  • F\mathbf{F} focus
  • PF=a(1−e)\mathbf{PF} = a(1 - e) periapsis distance (shortest distance from F\mathbf{F})
  • AF=a(1+e)\mathbf{AF} = a(1 + e) apoapsis distance (longest distance from F\mathbf{F})

Kepler’s Third Law:

T2=4π2GMa3T^2 = \frac{4\pi^2}{GM}a^3

Vis-Viva Equation:

v2=GM(2r−1a)v^2 = GM\left(\frac{2}{r} - \frac{1}{a}\right)

Wien’s Displacement Law:

λmax⁡T=constant\lambda_{\max}T = \mathrm{constant}

Stephan-Boltzmann Law:

L=4πR2σT4L = 4\pi R^2\sigma T^4

Brightness (Intensity):

b=L4πd2b = \frac{L}{4\pi d^2}

Magnitudes:

b1b0=10−0.4(m1−m0)\frac{b_1}{b_0} = 10^{-0.4(m_1 - m_0)}
m−M=5log⁡(d10)m - \mathcal{M} = 5\log\left(\frac{d}{10}\right)

Distance-Parallax Relation:

d=1pd = \frac{1}{p}

Rayleigh Criterion:

θ=1.22λD\theta = \frac{1.22\lambda}{D}

Redshift:

z=Δλλemit≈vcz = \frac{\Delta\lambda}{\lambda_{\mathrm{emit}}} \approx \frac{v}{c}

Hubble’s Law:

v=H0dv = H_0 d
Note for markers

Astro Round 2 2025 Paper 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. Units should be present on final answers when appropriate.
  • There are multiple ways to solve some of the questions; please accept all good solutions that arrive at the correct answer. Students getting the answer in a box\boxed{\text{box}} will get all the marks available for that calculation / part of the question (as indicated in red), so long as there are no unphysical / nonsensical steps or assumptions made (students may not explicitly calculate the intermediate stages and should not be penalised for this so long as their argument is clear).

In these solutions a plain [1] is a marking point and a bold [n] is the total for that calculation or part (printed in red in the source).

Условие

When a ray of light passes near to a massive body, the ray is deflected towards it by a very small angle due to the body’s gravity. This effect is known as gravitational lensing. The angle of deflection δ\delta is given by the formula

δ=4GMbc2 ,\delta = \frac{4GM}{bc^2}\ ,

where bb is the impact parameter, defined as the distance of closest approach between the ray’s original trajectory and the lensing mass.

One particularly interesting example of this phenomenon is Gravitational Microlensing, where the body causing the deflection is a relatively small mass such as a star or planet. This allows us to detect objects which are too dim to observe directly, such as exoplanets and brown dwarfs. In this question, we will examine how microlensing can be used to discover exoplanets by studying the gravitational interaction of light with the planet and its host star.

Left panel: observer O₁ on plane P_O, lens L on plane P_L and source S on one horizontal line; distances D_L (O₁ to L), D_LS (L to S) and D_S (O₁ to S) marked above; two rays from S bend at distance b above and below L towards O₁, arriving at angle θ_E on each side, with the deflection angle δ marked. Right panel: observer O₂ displaced a distance a below O₁ on P_O; rays from S pass the lens plane at b₋ above L and b₊ below L and reach O₂ at angles θ₋ and θ₊; a dotted line from O₂ to S makes the angle φ with the direction to L.
Figure 6: The lensing setup in both the aligned (left panel) and unaligned (right panel) cases. Note that the diagrams have been greatly scaled up in the vertical direction to make them visible, and in reality all rays are almost parallel. Credit: Ben Woodrow
Light curve titled OGLE-2012-BLG-0406: I magnitude (inverted axis, 15.5 to 17) against HJD − 2450000 (about 5950 to 6250). The baseline is near 16.35 on the left, the curve brightens smoothly to a peak of about 15.55 near 6140 and fades to about 16.25 by 6240; a sharp anomaly of points reaching about 15.4 appears near 6115–6120. A thin magenta model curve runs through the data points.
Figure 7: The light curve from the microlensing event OGLE-2012-BLG-0406, showing the variation in apparent magnitude against time in days. Credit: Udalski (2018).

a. (7 т.)

First, we will consider the scenario where the source SS, the lensing mass LL, and the observer O1O_1 are directly aligned, as shown in the left of Figure 6. This is an especially interesting case, as light from the source is able to reach the observer by passing around the source in any direction, creating a circular image known as an Einstein Ring, with angular radius θE\theta_E. We will assume that the lensing deflection occurs instantaneously at the point where the light passes though the lensing plane PLP_L. Since all the angles involved are extremely small, the impact parameter bb is simply the distance between this point and LL.

(i) Show that the Einstein radius is given by the formula

θE=4GMc2⋅DLSDSDL .\theta_E = \sqrt{\frac{4GM}{c^2}\cdot\frac{D_{LS}}{D_SD_L}}\ .

[4 т.]

(ii) Calculate the Einstein radius for a hypothetical Jupiter-sized exoplanet in a system with parallax 0.1960.196 milliarcseconds (mas), lensing light from a source star with parallax 0.0870.087 mas. Jupiter has a mass of 318 M⊕318\ M_{\oplus}. [3 т.]

b. (11 т.)

We will now consider how the lensed source will appear to an observer O2O_2, still situated in the plane POP_O, but now at a distance aa from O1O_1. In this case, instead of seeing the full Einstein Ring around the lens, the observer will see two point images at angles θ+\theta_+ and θ−\theta_-, one each side of the lens. The situation is shown in the right panel of Figure 6. This a much more typical scenario, as perfect alignments like the one in the previous part are extremely rare.

(i) Find an equation which must be satisfied by each of the angles θ±\theta_{\pm}. Hence, find show that θ+\theta_+ in terms of θE\theta_E and the Source-Observer-Lens angle φ\varphi is given by

θ+=12(φ+φ2+4θE2)\theta_+ = \frac{1}{2}\left(\varphi + \sqrt{\varphi^2 + 4\theta_E^2}\right)

and find an equivalent formula for θ−\theta_-. [6 т.]

(ii) Determine the maximum value of the angular displacement of the image at θ+\theta_+ from the unlensed position of the source as φ\varphi varies, and the corresponding value of φ\varphi. [4 т.]

(iii) What is the smallest diameter of telescope which would be able to resolve this maximal displacement for the hypothetical exoplanet mentioned earlier? [1 т.]

As you have just seen, the deflection caused by typically sized exoplanets is typically not directly observable by conventional optical means. Fortunately, the lensing also has a secondary effect of magnifying the brightness of the source, which is much more easily detected.

c. (15 т.)

We will now attempt to calculate the size of the amplification effect caused by the lensing.

(i) Find expressions for aa and the impact parameters b±b_{\pm} in terms of φ\varphi, θE\theta_E and the various DD. [3 т.]

(ii) Consider changing φ\varphi by a small increment dφ\mathrm{d}\varphi. Determine the corresponding changes da\mathrm{d}a and db±\mathrm{d}b_{\pm}. [3 т.]

(iii) By considering the total power incident on the annulus of points in POP_O between aa and a+daa + \mathrm{d}a with and without the lensing effect, determine the brightness of each of the two images compared to the unlensed brightness of the source. Give your answer in terms of the ratio u=φθEu = \frac{\varphi}{\theta_E}. [6 т.]

(iv) Assuming that the observer cannot resolve the two images, show that the total amplification factor is given by

A=u2+2uu2+4 .A = \frac{u^2 + 2}{u\sqrt{u^2 + 4}}\ .

[1 т.]

(v) For the same hypothetical exoplanet considered earlier, calculate the percentage increase in source brightness due to the lensing effect given φ=0.07\varphi = 0.07 mas. [2 т.]

This increase in brightness is much more easily detected than the change in image position angle found earlier, and so is the focus of many astronomical surveys.

d. (7 т.)

In 2012, researchers at the Optical Gravitational Lensing Experiment (OGLE) studied a microlensing event caused by a star and its exoplanet lensing the light from a more distant star. The light curve is shown in Figure 7. Most of the curve is a typical single source microlensing event with the star as the lens, as we considered in b. earlier. The anomaly at around t=6130t = 6130 is due to interaction with the exoplanet. As the source and lens move across the sky relative to each other, the value of uu changes, causing the variation in the brightness of the source. We will assume that the source and lens are moving with a constant relative angular velocity.

(i) Using values taken from Figure 7, a suitable numerical method and the formula given above for AA, determine the minimum value of uu over the course of this lensing interaction. [4 т.]

(ii) Determine the Einstein crossing time tEt_E, defined as the time taken for the source and lens to move relative to each other by an angle θE\theta_E. [3 т.]

These parameters describing the geometry of the microlensing event make it possible to fit a suitable model for a binary lens to match the anomaly seen in the data and determine the position and mass of the exoplanet.

Отговори

Решение

Questions proposed by

END OF PAPER

Questions proposed by:
James Kennedy (University of Oxford)
Charlotte Stevenson (University of Oxford)
Ben Woodrow (University of Oxford)
Dr Alex Calverley (Surbiton High School)


Оригинал в Архива: BAAO_R2_2025.pdf · официални решения: BAAO_R2_2025_solutions.pdf