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Regularized phase-space volume for the three-body problem

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Abstract

The micro-canonical phase-space volume for the three-body problem is an elementary quantity of intrinsic interest, and within the flux-based statistical theory, it sets the scale of the disintegration time. While the bare phase-volume diverges, we show that a regularized version can be defined by subtracting a reference phase-volume, which is associated with hierarchical configurations. The reference quantity, also known as a counter-term, can be chosen from a 1-parameter class. The regularized phase-volume of a given (negative) total energy, \({{\bar{\sigma }}}(E)\), is evaluated. First, it is reduced to a function of the masses only, which is sensitive to the choice of a regularization scheme only through an additive constant. Then, analytic integration is used to reduce the integration to a sphere, known as shape sphere. Finally, the remaining integral is evaluated numerically and presented by a contour plot in parameter space. Regularized phase-volumes are presented for both the planar three-body system and the full 3d system. In the test mass limit, the regularized phase-volume is found to become negative, thereby signaling the breakdown of the non-hierarchical statistical theory. This work opens the road to the evaluation of \({{\bar{\sigma }}}(E,L)\), where L is the total angular momentum, and in turn to comparison with simulation determined disintegration times.

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Notes

  1. Whenever the reader is unsure about whether we are using the (original) position variables (r) or the rescaled position variables \(({{\tilde{r}}})\), the appropriate factors of Energy (|E|) can be reinstated by dimensional analysis.

  2. We get the first equality by multiplying the third row by \(\frac{m_3}{M}\), then adding to it \(\frac{m_1}{M}\) times first row plus \(\frac{m_2}{M}\) times second row.

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Acknowledgements

Part of this research was supported by the Israel Science Foundation (Grant No. 1345/21). The work of S.M. was supported by the National Research Foundation of Korea grant NRF-2019R1A2C2084608. S.M. would like to thank the organizers of both ‘New Frontiers in Quantum Field Theory and String Theory’ and ‘Advances in Theoretical Physics 2022’ workshops for hospitality while this work was in progress.

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Correspondence to Yogesh Dandekar.

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Appendices

A Compensator evaluation

In this appendix, we detail the evaluation of the compensator (35). In fact, we provide two derivations.

The first way involves a reflection symmetry

$$\begin{aligned} \Delta {{\hat{\sigma }}}= & {} \frac{8}{\pi ^2} \int _{1/2}^\infty du_B \int _{1/2}^\infty du_F \int _{-1/2}^{u_F-1} d\epsilon \, \frac{\sqrt{u_B+\epsilon } \,\sqrt{u_F-1-\epsilon }}{u_B^4 \, u_F^4} \nonumber \\= & {} \frac{1}{2}\cdot \frac{8}{\pi ^2} \int _{1/2}^\infty du_B \int _{1/2}^\infty du_F \int _{-u_B}^{u_F-1} d\epsilon \, \frac{\sqrt{u_B+\epsilon } \,\sqrt{u_F-1-\epsilon }}{u_B^4 \, u_F^4} \nonumber \\= & {} \frac{1}{2}\cdot \frac{8}{\pi ^2} \cdot \frac{5 \pi }{9} = \frac{20}{9\pi } ~. \end{aligned}$$
(67)

The second way involves a direct integration with a convenient ordering of the three integrations

$$\begin{aligned} \Delta {{\hat{\sigma }}}= & {} \frac{8}{\pi ^2} \int _{1/2}^\infty \frac{du_B}{u_B^4} \int _{-1/2}^\infty d\epsilon \, \sqrt{u_B+\epsilon } \int _{1+\epsilon }^\infty du_F \, \frac{\sqrt{u_F-1-\epsilon }}{u_F^4} \nonumber \\= & {} \frac{8}{\pi ^2} \int _{1/2}^\infty \frac{du_B}{u_B^4} \int _{-1/2}^\infty d\epsilon \sqrt{u_B+\epsilon } \, \frac{\pi }{16} (1+\epsilon )^{-5/2} \nonumber \\= & {} \frac{8}{\pi ^2} \int _{1/2}^\infty \frac{du_B}{u_B^4} \, \frac{\pi }{24} \frac{(2 u_B-1)^{3/2}-1}{u_B-1} \nonumber \\= & {} \frac{32}{3 \pi } \int _0^\infty du \, \frac{u (u^2+u+1)}{(u^2+1)^4(u+1)} = \frac{20}{9 \pi } \end{aligned}$$
(68)

where in passing to the fourth line, we have changed variables according to \(u^2=2 u_B-1\).

B Planar reduction

In this appendix, we derive (36). We start with the following rewriting of the LHS:

$$\begin{aligned} \begin{aligned} \left( \prod _{c=1}^3 d^3 r_c \right) \, \delta ^{(3)}(\vec R_\textrm{CM})&= \left( \prod _{c=1}^3 d^2 r_c \right) \, dz_1 \, dz_2 \, dz_3 \, \delta ^{(2)}(\vec R_\textrm{CM}) \, \delta \left( \frac{1}{M}(m_1 z_1 + m_2 z_2 + m_3 z_3)\right) \\&=\left( \prod _{c=1}^3 d^2 r_c \right) \, dz_1 \, dz_2 \, \delta ^{(2)}(\vec R_\textrm{CM}) \left( \frac{M}{m_3}\right) ~. \end{aligned} \end{aligned}$$
(69)

Next, we express \(dz_1\) and \(dz_2\) in terms of rotations in the \(x-y\) plane

$$\begin{aligned} \begin{aligned} dz_1&= d\vec \phi \times \vec r_1 \\ dz_2&= d\vec \phi \times \vec r_2 ~, \end{aligned} \end{aligned}$$
(70)

where \(d\vec \phi \) is an infinitesimal vector in the \(x-y\) plane. Since

$$\begin{aligned} \begin{bmatrix} dz_1 \\ dz_2 \end{bmatrix} = \begin{bmatrix} y_1 &{} -x_1 \\ y_2 &{} -x_2 \end{bmatrix} \begin{bmatrix} \hbox {d}\phi _x \\ \hbox {d}\phi _y \end{bmatrix} ~, \end{aligned}$$
(71)

we have

$$\begin{aligned} dz_1 dz_2 = (x_1y_2-y_1x_2)\hbox {d}\phi _x \hbox {d}\phi _y ~. \end{aligned}$$
(72)

Area of the triangle formed by the three bodies is given by the determinant

$$\begin{aligned} A= \frac{1}{2}\begin{vmatrix} x_1&y_1&1\\ x_2&y_2&1\\ x_3&y_3&1 \end{vmatrix} ~, \end{aligned}$$
(73)

which can be reduced using the following stepsFootnote 2

$$\begin{aligned} \begin{aligned} A&= \frac{1}{2}\frac{M}{m_3}\begin{vmatrix} x_1&y_1&1\\ x_2&y_2&1\\ \frac{m_1 x_1 + m_2 x_2 + m_3 x_3}{M}&\frac{m_1 y_1 + m_2 y_2 + m_3 y_3}{M}&1 \end{vmatrix} \\ {}&= \frac{1}{2}\frac{M}{m_3}\begin{vmatrix} x_1&y_1&1\\ x_2&y_2&1\\ 0&0&1 \end{vmatrix}\\ {}&= \frac{1}{2}\frac{M}{m_3} (x_1 y_2-y_1 x_2) \end{aligned} \end{aligned}$$
(74)

Using (72) and (74) we get

$$\begin{aligned} dz_1 dz_2 = 2A ~\frac{m_3}{M} ~\hbox {d}\phi _x \hbox {d}\phi _y \end{aligned}$$
(75)

Substituting (75) in (69), we get

$$\begin{aligned} \begin{aligned} \left( \prod _{c=1}^3 d^3 r_c \right) \, \delta ^{(3)}(\vec R_\textrm{CM})&= 2A \left( \prod _{c=1}^3 d^2 r_c \right) \, \delta ^{(2)}(\vec R_\textrm{CM})~ \hbox {d}\phi _x \hbox {d}\phi _y\\ {}&= 2A \left( \prod _{c=1}^3 d^2 r_c \right) \, \delta ^{(2)}(\vec R_\textrm{CM})~ \hbox {d}\Omega \end{aligned} \end{aligned}$$
(76)

where we rewrite \(\hbox {d}\phi _x\hbox {d}\phi _y\) as \(\hbox {d}\Omega \), which is the differential solid angle on the unit sphere. We have thus derived (36).

C Expressions for potential and triangle area

In this appendix, we derive the expressions for AV in terms of \(r,\theta ,\phi ,\psi \) coordinates. For this, we need the expressions for the relative distances between the three bodies, i.e., \(r_{12},r_{13},r_{23}\). First, we express them in terms of w variables defined in (38)

$$\begin{aligned} r_{12} = ~\left| \frac{w-\eta {\bar{w}}}{1-\eta } \right| \quad ,\quad r_{13} = ~\left| \frac{w-{\bar{\eta }} {\bar{w}}}{1-{\bar{\eta }}} \right| \quad ,\quad r_{23} = ~\left| \frac{w- {\bar{w}}}{\eta -{\bar{\eta }}}\right| \end{aligned}$$
(77)

where we use the following notation: \(\eta =e^{j\frac{2\pi }{3}},~{\bar{\eta }}=e^{-j\frac{2\pi }{3}},~\bar{w}=w/.\{j\rightarrow -j\}\) and the absolute values are calculated with respect to i. Using (42), we rewrite in terms of \(r,\theta ,\phi ,\psi \) coordinates

$$\begin{aligned} \begin{aligned} r_{12}&= r \sqrt{1-\sin \theta \cos \left( \phi +\frac{2\pi }{3}\right) } \quad , \quad r_{13} = r \sqrt{1-\sin \theta \cos \left( \phi -\frac{2\pi }{3}\right) }\\ r_{23}&= r \sqrt{1-\sin \theta \cos \phi } \end{aligned} \end{aligned}$$
(78)

From (78), it is straightforward to derive expression for V in (46).

To derive the expression for A in (45), we use the formula

$$\begin{aligned} A = \frac{1}{4} \sqrt{(r_{12}^2+r_{13}^2+r_{23}^2)^2-2(r_{12}^4+r_{13}^4+r_{23}^4)} \end{aligned}$$
(79)

and substitute (78) to derive (45).

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Dandekar, Y., Kol, B., Lederer, L. et al. Regularized phase-space volume for the three-body problem. Celest Mech Dyn Astron 134, 55 (2022). https://doi.org/10.1007/s10569-022-10108-1

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