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MODELING COLLISIONAL CASCADES IN DEBRIS DISKS: STEEP DUST-SIZE DISTRIBUTIONS

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Published 2012 July 6 © 2012. The American Astronomical Society. All rights reserved.
, , Citation András Gáspár et al 2012 ApJ 754 74 DOI 10.1088/0004-637X/754/1/74

0004-637X/754/1/74

ABSTRACT

We explore the evolution of the mass distribution of dust in collision-dominated debris disks, using the collisional code introduced in our previous paper. We analyze the equilibrium distribution and its dependence on model parameters by evolving over 100 models to 10 Gyr. With our numerical models, we confirm that systems reach collisional equilibrium with a mass distribution that is steeper than the traditional solution by Dohnanyi. Our model yields a quasi-steady-state slope of n(m) ∼ m−1.88 [n(a) ∼ a−3.65] as a robust solution for a wide range of possible model parameters. We also show that a simple power-law function can be an appropriate approximation for the mass distribution of particles in certain regimes. The steeper solution has observable effects in the submillimeter and millimeter wavelength regimes of the electromagnetic spectrum. We assemble data for nine debris disks that have been observed at these wavelengths and, using a simplified absorption efficiency model, show that the predicted slope of the particle-mass distribution generates spectral energy distributions that are in agreement with the observed ones.

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1. INTRODUCTION

The total mass within debris disks as well as the infrared excess emission produced by their dust is generally calculated assuming the analytic estimate of the distribution of masses in the asteroid belt by Dohnanyi (1969). This solution predicts that the sizes follow a power law, with their numbers increasing with decreasing size a as n(a) ∼ a−3.5. However, a number of recent efforts to model observations of debris disks have found it necessary to adopt steeper slopes (Krist et al. 2010; Golimowski et al. 2011).

Durda & Dermott (1997) and O'Brien & Greenberg (2003) have shown numerically and analytically that a steep tensile strength curve, i.e., the function that gives the minimum energy required to disrupt a body catastrophically (see, e.g., Holsapple et al. 2002; Benz & Asphaug 1999; Gáspár et al. 2012), results in a steeper quasi-steady-state distribution than the traditional solution. Collisional models of the dust in debris disks (Thébault et al. 2003; Krivov et al. 2005; Thébault & Augereau 2007; Löhne et al. 2008; Müller et al. 2010; Wyatt et al. 2011) have also shown that the dust particles will settle with a size distribution slope larger than 3.6, on top of which additional structures appear. This steeper distribution has readily observable effects at the far-IR and submillimeter wavelengths. It also results in higher total dust mass and lower planetesimal mass estimates for the systems. However, these results are often disregarded in observational studies. Instead, the traditional Dohnanyi (1969) slope of mass distribution is used, likely due to the complexity of the numerical models, the superposed wavy structures on the distributions, and their uncertain regimes of applicability.

In this paper, we investigate the slope of the mass distribution and the physical parameters that influence it with the numerical code introduced in Gáspár et al. (2012, hereafter Paper I). Our code calculates the evolution of the particle-mass distribution in collisional systems, taking into account both erosive and catastrophic collisions. In Section 2, we introduce models for the numerical analysis of the collisional cascades and give our findings. In Section 3, we analyze the ranges where a simple power-law function is an appropriate approximation for the mass distribution of particles. In Section 4, we compare our model's properties to the assumptions of previous analytic solutions, while in Section 5, we generate a set of synthetic spectra in order to analyze the effects certain distribution parameters have on different parts of the spectral energy distributions (SEDs). In Section 6, we introduce a simple relation between the Rayleigh–Jeans part of the SEDs and the particle-size distribution. In Section 7, we compare our results to the observed far-IR and submillimeter data for nine sources.

2. NUMERICAL MODELING

In this section, we analyze the dust distribution with our full numerical code (Paper I). We run a set of numerical models to study the evolution of the slope of the distribution function and its dependence on the model parameters. We investigate the time required for the distribution to settle into its quasi-steady state and, with a wide coverage of the parameter space, we also examine the robustness of the solution.

2.1. Evolution of the Reference Model

We set up a reference debris disk as a basis for comparison to all other model runs. This model consists of a moderately dense debris disk situated at 25 AU around an A0 spectral-type star, with a width and height of 2.5 AU. This radial distance ensures a moderate evolution speed. The peak emission is in the mid-infrared, with a Rayleigh–Jeans tail in the far-infrared regime, which is the primary imaging window for the Herschel Space Telescope. The total mass in the debris disk is 1 M, distributed between minimum and maximum particle masses that correspond to radii of 5 nm and 1000 km, when assuming a bulk density of 2.7 g cm−3. We summarize the disk parameters of the reference model in Table 1. We evolve the reference model for 10 Gyr.

Table 1. Numerical, Collisional, and System Parameters of Our Reference Model

Variable Description Fiducial Value
System Variables
ρ Bulk density of particles....................................................................... 2.7 g cm−3
mmin Mass of the smallest particles in the system........................................ 1.42 × 10−21 kg
mmax Mass of the largest particles in the system........................................... 1.13 × 1022 kg
Mtot Total mass within the debris ring......................................................... 1 M
η0 Initial power-law distribution of particle masses................................. 1.87
R Distance of the debris ring from the star.............................................. 25 AU
ΔR Width of the debris ring........................................................................ 2.5 AU
h Height of the debris ring...................................................................... 2.5 AU
Sp Spectral type of the star........................................................................ A0
Collisional Variables
γ Redistribution power law...................................................................... 11/6
βX Power exponent in X particle equation................................................ 1.24
α Scaling constant in Mcr........................................................................ 2.7 × 10−6
b Power-law exponent in Mcr equation................................................... 1.23
fM Interpolation boundary for erosive collisions....................................... 10−4
fY Fraction of Y/Mcr................................................................................ 0.2
fmaxX Largest fraction of Y/X at super catastrophic collision boundary...... 0.5
Qsc Total scaling of the Q* strength curve................................................. 1
S Scaling of the strength regime of the Q* strength curve..................... 3.5 × 107 erg g−1
G Scaling of the gravity regime of the Q* strength curve....................... 0.3 erg cm3 g−2
s Power exponent of the strength regime of the Q* strength curve........ −0.38
g Power exponent of the gravity regime of the Q* strength curve.......... 1.36
Numerical Parameters
δ Neighboring grid point mass ratio 1.104
Θ Constant in smoothing weight for large-mass collisional probability 106mmax
P Exponent in smoothing weight for large-mass collisional probability 16

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In Figure 1, we show the evolution of the particle distribution, plotting it at six different points in time up to 10 Gyr. On the vertical axis we plot log10[n(m) × m2], which can be related to the "mass/bin" that is frequently used in other simulations. Even though the number densities decrease with increasing particle masses, the mass distribution increases toward the larger masses in this representation, as long as the mass distribution slope is smaller than 2.

Figure 1.

Figure 1. Particle-mass distribution of the reference model plotted at various points in time.

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The smallest particles reach collisional equilibrium first, roughly at 1 Myr, followed by larger particle sizes as the system evolves. After 50–100 Myr of evolution, the upper, gravity-dominated part of the distribution (m > 1013 kg) also reaches equilibrium. The distribution maintains its slope for masses below 1010 kg, which roughly corresponds to a planetesimal radius of 100 m. The kink in the distribution at the upper end is due to the change in the strength curve slope (O'Brien & Greenberg 2005; Bottke et al. 2005).

Structures in the distribution slope, such as waves, may in principle occur at the low-mass end when assuming softer material properties or higher collision velocities (see Section 3). The distribution may also acquire some curvature (see Paper I). Because of these effects, we evaluate the average slope of the distribution by fitting a power law over a large-mass range, but one that remains below the kink in the distribution. Specifically, we fit the slope between masses 10−8 and 104 kg, which roughly correspond to sizes of 0.1 mm and 1 m.

We next examine the dependence of the quasi-steady-state distribution slope on the initial conditions, i.e., the initial-mass distribution slope η0 and the initial total mass in the disk Mtot. Figure 2 shows the evolution of the particle-mass distribution and its slope as a function of these initial conditions. The left panels show the mass distribution after 10 Gyr for different values of the two input parameters, while the right panels show the evolution of the dust-mass distribution slope. Variations in the initial slope, η0, do not affect the final slope value, although the high-mass end evolves differently or reaches equilibrium at different timescales. A distribution with less dust initially (η0 < 1.87) also takes more time to reach equilibrium. A shallow distribution with an initial slope of η0 = 1.5 takes as much as ∼1 Gyr to reach equilibrium, although such initial distribution slopes are unlikely. As shown by Löhne et al. (2008), the evolution of the particle-mass distribution is scalable by the total mass (or number densities of particles), which is what we see in the bottom two panels of Figure 2. All systems with different initial masses reach the same equilibrium mass distribution, but on different timescales. More massive systems evolve on shorter timescales, thus reaching their equilibrium more quickly, while less massive systems evolve more slowly.

Figure 2.

Figure 2. Left panels: particle-mass distribution at 10 Gyr, when varying the initial-mass distribution slope (top) and the total mass of the system (bottom). Right panels: evolution of the dust-mass distribution slopes when varying the initial-mass distribution slope (top) and the total mass of the system (bottom). The quasi-steady-state distribution slope is practically independent of these initial conditions.

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2.2. The Dependence of the Quasi-steady-state Distribution Function on the Collision Parameters

The parameters that describe the outcomes of collisions, in principle, should be roughly the same for all collisional systems. They are the fragmentation constants and the parameters of the strength curve (Benz & Asphaug 1999). To investigate their effects on the evolution of the particle-mass distribution, we vary their nominal values and evolve the models to the same 10 Gyr, as we did for the reference model.

We give here a detailed analysis of the effects of varying only 5 of the 12 parameters (α, b, Qsc, s, S), as the remaining seven (γ, βX, fY, fmaxX, fM, g, G) have no significant effects (see Table 1 for the description of these parameters).

In Figure 3, we plot the resulting mass distributions when varying the cratered mass parameters α and b (Koschny & Grün 2001a, 2001b). The parameter α is the total scaling and b is the exponent of the projectile's kinetic energy in the equation of the cratered mass

Equation (1)

As can be seen in Figure 3, the resulting mass distributions depend on the values of α and b only in the gravity-dominated regime. At these larger masses, our model is incomplete, because we do not include aggregation. When increasing α, i.e., basically softening the materials or increasing the effects of erosions, the number of eroded particles in the gravity-dominated regime increases rapidly. A similar effect can be observed when increasing the value of b. However, within reasonable values of α and b, the variation of the equilibrium particle-mass distribution slope in the dust mass regime is negligible.

Figure 3.

Figure 3. Particle-mass distribution at 10 Gyr, when varying the parameters α (left) and b (right) of the cratered mass (Equation (1)). Variations in the particle distribution only occur at large masses, the dust-mass distributions are the same for all models.

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In Figure 4, we plot the resulting distributions and the evolution of the dust distribution slope when we vary the parameters Qsc, S, and s. These are all variables in the tensile strength curve, which is given as (Benz & Asphaug 1999)

Equation (2)

The variable Qsc is a global scaling factor, S is the scaling of the strength-dominated regime, s is the power dependence on particle size of the strength-dominated regime, G is the scaling of the gravity-dominated regime, and g is the power dependence on particle size of the gravity-dominated regime. Variations in the gravity-dominated regime of the curve (G and g) do not have significant effects on the equilibrium dust-mass distribution, so we do not consider these parameters further. The tensile strength curve has been extensively studied for decades. However, as it is dependent on various material properties and the collisional velocity (Stewart & Leinhardt 2009; Leinhardt & Stewart 2012), its parameters do not have universally applicable values. Determining the tensile strength curve at large and small sizes is also extremely difficult experimentally.

Figure 4.

Figure 4. Left panels: particle-mass distribution at 10 Gyr, when varying the values of the tensile strength curve parameters Qsc, S, and s. Right panels: evolution of the dust-mass distribution slopes when varying the values of the same parameters.

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The slope s of the strength curve in the strength-dominated regime depends on the Weibull flaw-size distribution. Its measured values range anywhere between −0.7 and −0.3 (Holsapple et al. 2002). Steeper values of s make smaller materials harder to disrupt, which results in a steeper dust distribution slope. At s = 1.0, the smallest particles are hard enough to resist catastrophic disruption even when the projectile mass equals the target mass. This results in a mass distribution with a slope equal to the redistribution slope γ = 1.83 at the smallest scales, while in the fitted region it is significantly steeper. At s = 0.6, the smallest particles are still able to destroy each other and generate a dust distribution slope that is close to 1.91.

The scaling constants of the tensile strength curve are the dominant parameters in the evolution toward the quasi-steady-state distribution. When reducing the complete tensile strength curve scaling Qsc, wave structures form more easily, as a particle becomes capable of affecting the evolution of particles much larger than itself (see Paper I). When upscaling the tensile strength curve, the quasi-steady-state distribution slope starts to resemble the redistribution slope, as it is the particle redistributions that leads the evolution of the particle-mass distribution. When varying the scaling of only the strength side of the curve S, similar effects can be seen.

We have shown that drastic offsets in the collision parameter values result in slight changes to the quasi-steady-state mass distribution slope. We conclude that, for all reasonable values of the collisional parameters, the quasi-steady-state dust-mass distribution slope is larger or equal to 1.88.

2.3. The Dependence of the Distribution Function on System Variables

There are a number of parameters that can change from one collisional system to another: the material density ρ, the minimum and the maximum particle mass in the system mmin and mmax, the radial distance R, height h, and width ΔR of the disk, and the spectral type of the central star. All these parameters affect three properties of the collisional model: the blowout mass, the collisional velocity, and the number density of particles. Varying these parameters will change the timescale of the evolution and affect the quasi-steady-state distribution slope. In this subsection, we analyze the effects of varying the radial distance on the equilibrium mass distribution through the dependence of the collisional velocity on radius. Modifying either disk parameters ΔR and h or the spectral type of the star would have similar effects. We defer discussion of the variations in the timescales to a future paper.

In the left panel of Figure 5, we show the effects of varying the radial distance, R, on the mass distribution evolved to 10 Gyr. Decreasing the radial distance will increase the collisional velocity, resulting in the appearance of waves at the small-mass end of the distribution. It also generates a much more pronounced kink at the high-mass end. On the other hand, when the velocity is decreased at large radii, the low-mass end of the distribution starts resembling the redistribution function, as smaller particles are not destroyed due to the lower energy collisions. Moreover, no kink is produced at the high-mass end. In the right panel of Figure 5, we show the evolution of the particle-mass distribution slope as a function of the collisional velocity. For high-velocity collisions, the waves render the fitting of a single-mass distribution slope ill constructed but the underlying slope of the wavy-mass distribution is slightly steeper than for the smaller collisional velocity case.

Figure 5.

Figure 5. Left panel: particle-mass distribution at 10 Gyr, when varying the value of the radial distance of the disk. Right panel: evolution of the dust-mass distribution slopes when varying the same parameter.

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2.4. The Dependence of the Distribution Function on Numerical Parameters

We discuss here the effects of three non-physical variables that appear in the numerical algorithm. They are: the mass ratio δ between neighboring grid points and the parameters of the large particle collisional cross-section smoothing formula, Θ and p (see Paper I). In Figure 6, we plot the distribution of the model with varying values of δ at 10 Gyr (left panel) and the evolution in the slope of the dust distribution (right panel). The evolution of the dust distribution is affected by the number of grid points we use, converging at δ = 1.13; this corresponds to 801 grid points between our mmin and mmax mass range. Using a lower number of grid points leads to errors in the numerical integration for the redistribution, leading to an offset larger than 7% for the smallest particles in the system, when only using half as many grid points. We find that the dust distribution slope is practically independent of the smoothing variables Θ and p.

Figure 6.

Figure 6. Left panel: particle-mass distribution at 10 Gyr, when varying the resolution of the numerical model. Right panel: evolution of the dust-mass distribution slopes when varying the same parameter.

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2.5. The Time to Reach Quasi-steady State

In our model calculations, the dust distributions in the vast majority of cases reach quasi-steady state by 10–20 Myr and only in a few cases do they take somewhat longer. The characteristic time is less than 100 Myr for all realistic cases in agreement with previous studies (e.g., Wyatt et al. 2007; Löhne et al. 2008). This shows that, apart from second generation debris disks, the majority of debris disks around stars of ages over 100 Myr are most likely to be in collisional quasi-steady state, at least for the smallest particles (<1 cm). However, young and extended systems, such as β Pic (Smith & Terrile 1984; Vandenbussche et al. 2010), might not be near quasi-steady state at the outer parts of their disks, where interaction timescales are longer.

2.6. The Robustness of the Solution

One of the most surprising results of the wide range of numerical models we computed is the robustness of the quasi-steady-state distribution. Varying the values of the model parameters does not result in significant changes in the slope of the distributions. In Figure 7, we show the effect on the equilibrium slope of the dust-mass distribution function of varying each model parameter. We order the parameters on the horizontal axis as a function of decreasing magnitude of their effects. Parameters that had to be varied by many orders of magnitude to have effects on the equilibrium slope are analyzed in log space. The plot shows that the dominant parameter, by far, is the slope of the strength curve in the strength-dominated regime. This is followed by variables that affect the collisional velocity (ΔR and h) and the power b of the erosive cratered mass formula (Equation (1)). The plot also shows that neither of our arbitrarily chosen collision prescription constants have any significant effects on the outcome of the collisional cascade. The model runs predict an equilibrium dust-mass distribution slope of η = 1.88 ± 0.02 (ηa = 3.65 ± 0.05), taking the maximum offsets originating from the 50% variation in the model parameters test as our error.

Figure 7.

Figure 7. Effect on the equilibrium particle-mass and size distributions of varying each collisional and system variable by 50%.

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3. THE POWER-LAW APPROXIMATION OF THE MASS DISTRIBUTIONS

Due to the complexity of full numerical models and the varying amount of structures in the particle-mass distributions presented in the papers detailing them, it is still common practice for debris disk SEDs to be calculated and fitted to observed data assuming a simple power law for the mass distribution of particles. The applicability of a power-law distribution has never been probed systematically. Another issue within this simplification is that the value for the slope of the power law used is generally the traditional 11/6 (or 3.5 in size space) determined by Dohnanyi (1969), although this has already been proven to be only valid for the constant material tensile strength case by Durda & Dermott (1997) and O'Brien & Greenberg (2003). As we have shown in the preceding sections, a steeper distribution function of η = 1.88 ± 0.02 (ηa = 3.65 ± 0.05) is a more likely outcome when considering realistic conditions. Similar results have been found by Durda & Dermott (1997), O'Brien & Greenberg (2003), and Thébault & Augereau (2007), among others.

In this section, we investigate the extent to which a simple power law is a valid approximation for the mass distribution in debris disks. As we are evaluating the detectability of effects of deviations from a power-law mass distribution on the generated SEDs, we are only concerned with particles smaller than ∼1 mm in size. Deviations from a power law on this scale occur when waves appear superposed on the distribution itself, meaning the conditions that result in the formation of waves in the particle-mass distribution need to be studied.

3.1. Appearance of Waves in the Particle-mass Distribution

Waves appear superposed on the mass distribution due to the discontinuity at the low-mass cutoff. This behavior has been explained before as a result of the buildup of particles at the boundary (Campo Bagatin et al. 1994; Wyatt et al. 2011); however, examining the properties of the collisional equation (see Paper I) yields a different picture. In Figure 8, we plot the dμ integrand of the collisional equation

Equation (3)

which basically gives the amount of variations produced by a μ mass projectile for a certain m mass, either by μ removing m or adding it as an X fragment. In regimes marked with a "+" the effective changes in the number densities are positive, while in regimes marked with a "−" they are negative. With solid black lines we show the integrands for the m masses where the first dip of the waves are situated for the corresponding velocities. It is apparent that for these masses the peaks of the removal integrands are located exactly at the cutoff. The fact that they are peaks is obvious when comparing with the integrands of larger masses. If the distributions were continuous, this effect would smooth out, but with the cutoff located at the peak of the integrand, relatively more will be removed of mass m at the first dip than of other masses. We also note that the additive peaks of the minimum (cutoff) mass, shown with red solid curves, are not correlated with the location of the dip in the distribution (marked with a black solid tick mark), but shift as a function of the collision velocity. At higher collisional velocity, where waves are stronger, the largest number of cutoff particles are actually produced by the particles in the dip, which would provide a negative feedback according to the traditional picture, canceling the waves. Our analysis shows that positive feedback is not the dominant effect in the production of the waves.

Figure 8.

Figure 8. Integrands of Equation (3) for selected m masses in system with collisional velocities of 3 km s−1 (left panel) and 6 km s−1 (right panel). The solid black lines give the integrands for the mass at the first wave dip in each system (mwave), while the solid red lines give the integrands for the minimum mass in the system. The removal peak of the mwave integrand is at the cutoff, explaining the excess removal at the first dip in the waves. The tick marks show the location of the masses in the distribution for which integrands are displayed. See the text for detailed description of the formation of the wave structure.

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The location of the peak of the removal term (Term I in Paper I) is the determining factor in the formation of the waves, which can be given by solving

Equation (4)

where m gives the location of the first dip and M is given so that X(μ, M) ≡ m. Unfortunately, an analytic solution cannot be given, as the derivative is transcendent, but is easily solvable numerically. The variable that determines the solution will be X, which depends on the collisional velocity, the tensile strength law, and the value of mmin. For a given system, where mmin and the tensile strength law do not change as a function of radial location, the single variable determining the wavy structure is the collisional velocity. The minimum mass will change as a function stellar types and some material/velocity dependence of the tensile strength law can be expected between systems.

3.2. Constraining the Conditions for the Appearance of Waves in the Particle-mass Distribution

In Section 2, we have shown that variations in the proxies for the collisional velocity (such as disk radius) can in fact result in wavy size distributions, even within a narrow debris ring. Extended debris disks will be even more likely to have higher collisional velocities, as the particles with higher β values (but less than 0.5) get placed on high eccentricity orbits. These small particles from the inner rings will collide with the particles in the external rings with increased velocities due to the non-zero collisional angles (Thébault & Augereau 2007). To study the effects of variations only in the collisional velocity, we set the collisional velocity directly within our code to specific values, not changing any other parameters. We present the results from these runs in Figure 9. The figure shows that waves start to appear at collisional velocity values of 3 km s−1 and above.

Figure 9.

Figure 9. Particle-mass distribution at 10 Gyr, when varying the collisional velocity in the system. Waves start to appear at and above collisional velocities of 3 km s−1, when constraining all other parameters at their fiducial values. Note that the collisional velocity was adjusted by hand in these models and not determined by the system geometry as described in Paper I, in order to study the effects of only variations in the collisional velocity itself.

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The value of the orbital velocity for a particle on an elliptical orbit originating from Rin with a certain β value at Rout radius (where it will collide with a particle on a circular orbit) is

Equation (5)

The angle between the orbital velocities can be expressed as

Equation (6)

where

Equation (7)

Equation (8)

The collisional velocity is then

Equation (9)

where vo is the orbital velocity for the particle on a circular orbit at Rout.

We plot the values of this collisional velocity for particles originating from Rin = 10 AU and 50 AU in systems around a solar- and early-type star in Figure 10. We shade the collisional velocity region above our 3 km s−1 limit, where waves start to appear. As we can see, nearby rings at ΔR = 1 AU have low collisional velocities, reassuring that our prescription for a constant collisional velocity value in narrow debris rings is reasonable. We can also see that once we depart from the narrow ring assumption (ΔR > 10 AU), the collisional velocities do increase.

Figure 10.

Figure 10. Collisional velocity between particles originating from a radius of Rin and colliding with particles at radius Rout, with eccentricities calculated from their β values. We show cases for a solar-type star and an A0 spectral-type star, with Rin values of 10 and 50 AU.

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Around a solar-type star, particles originating from an inner radius of 10 AU are able to achieve collisional velocities of ∼3 km s−1; however, the particle-size range that is able to achieve this limit is very narrow, between 0.4 and 0.6 μm. Taking into account the dilution of these small particles within a limited narrow size range, we conclude that extended debris disks with inner boundaries outside of 10–15 AU around solar-type stars should be well approximated by a simple power-law mass (size) distribution function. In Paper I, we show a comparison run to Löhne et al. (2008) and Wyatt et al. (2011), assuming an extended disk between radii of 7.5 and 15 AU around a solar-type star. The runs by Wyatt et al. (2011) and our code show negligible/small amplitude waves, while Löhne et al. (2008) show moderate amplitude waves, likely due to their full three-dimensional modeling of the system, taking into account smaller particles originating from regions inward of 10 AU. These results confirm our analytic analysis on the conditions required to initiate waves in the dust particle-mass distribution.

We show the same analysis for early-type stars in the right panels of Figure 10. The collisional velocities of particles originating from 10 AU with particles on external circular orbits around an A0 spectral-type star will be significantly larger than our limit for a larger range of particle sizes (5–10 μm). Particles originating from orbits inside of 10 AU will definitely initiate waves in extended disks or external rings. However, particles originating from 50 AU will barely reach collisional velocities at or above our limit and for a limited range of particle sizes. We conclude that extended debris disks with inner boundaries outside of 50–60 AU around early-type stars should be well approximated by a simple power-law mass (size) distribution function.

Our one-dimensional "particle-in-a-box" numerical code adjusts the collisional velocities through the ring thickness and height (ΔR and h), and the resulting orbital inclinations for the particles. Our results are only moderately affected over the relatively narrow range of velocities obtained by varying them (see Figure 7). We modified the code (see above) to simulate the higher-velocity collisions with particles on elliptical orbits to determine a threshold for generation of waves in the particle distribution. However, our model cannot explore the nuances resulting from varying collisional velocities in extended systems (such as varying collisional rates and collisional outcomes), which could also play a role in the possible formation of substructures superposed on the generally steeper particle-size distributions (see, e.g., Krivov et al. 2005; Thébault & Augereau 2007; Löhne et al. 2008; Müller et al. 2010).

As stated at the end of Section 3.1, our generalization assumed a specific system (with same material properties and minimum particle mass). Although we explored varying the minimum particle mass when introducing different spectral-type central stars, both the tensile strength and the minimum mass may vary with material properties as well. In addition to minerals such as basalt, it is likely that grains in the outer zones of debris disks contain significant amounts of ice. The mechanical properties of icy grains are explored by Benz & Asphaug (1999) and Leinhardt & Stewart (2009), yielding roughly a factor of three in difference between the tensile strength of basalt and ice. Given the relative insensitivity of our results to the scaling of the grain strength curve (Qsc, see Figure 7), these properties are similar enough that our basic conclusions about the grain size distribution and region of applicability of the power-law approximation to it are essentially unchanged even outside of the iceline.

4. COMPARISON TO PREVIOUS ANALYTIC APPROACHES

The slope of the size distribution slope in collisional cascades has been investigated with analytic approaches with increasing complexity since the pioneering work of Dohnanyi (1969). His assumptions of self-similar fragmentation, constant material strength, and collision rates proportional to the geometric cross section led to the well known and now widely used steady-state size distribution slope of ηm = 11/6 (ηa = 3.5). The validity of his assumptions has been investigated in a number of analytic studies. Tanaka et al. (1996) found that varying the power of the collisional cross section (mν, where ν = 2/3 for a simple geometric cross section) will set the steady-state distribution slope as ηm = (ν + 3)/2. Such non-geometric cross sections (collision rates) can be the results of mass-weighted collision probabilities, varying amounts of grain porosity, mass-dependent collisional velocities, etc. O'Brien & Greenberg (2003) investigated whether a non-constant tensile strength value, defined by a power law with slope of s, will affect the steady-state particle-size distribution. They found a linear relationship between the two power-law slopes, yielding a steady-state solution producing more small particles than the traditional Dohnanyi (1969) solution, when considering realistic tensile strength slopes. An analytic solution similar to the one by O'Brien & Greenberg (2003) was presented in Wyatt et al. (2011), who also analyzed their equations numerically, revealing substructures superimposed on the power-law size distributions. Belyaev & Rafikov (2011) expanded on the O'Brien & Greenberg (2003) model by allowing a variable largest fragment mass to target mass ratio (X/M in our model), following the Fujiwara et al. (1977) experimental results. Belyaev & Rafikov (2011) found a particle distribution that could not be described by a single power law, rather by a slowly varying, mass-dependent power-law function. We summarize the characteristic properties of these analytic models in Table 2. A common issue with all of these analytic solutions is that they assume a steady-state system, meaning that the mass flux through mass m is zero [∂F(m)/∂m = 0]. In reality, without mass input at the high-mass end, the systems lose mass and decay, meaning the mass flux is never zero in a system, but rather is a time- and mass-dependent variable. The solution of the cascade is actually an eigenvalue problem, which is difficult to solve analytically.

Table 2. Comparing the Properties of Analytic Solutions with Our Numerical Model

Model Collision Rate X/M Q*D Redistribution $\frac{d \ln n(m)}{d \ln m}$
Dohnanyi (1969) m2/3 Constant Constant Power law 11/6
Tanaka et al. (1996) mν Constant Constant Power law (ν + 3)/2
O'Brien & Greenberg (2003) m2/3 Constant Power law Power law (11 + s)/(6 + s)
Belyaev & Rafikov (2011) m2/3 Variable Power law Power law Slowly varying function of m
This work Variable Variable Power law Power law Function of model parameters,
          largely robust around −1.88

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Our numerical code allows for investigating the quasi-steady-state [∂F(m)/∂m ≠ 0] solution of collisional cascades, without the aforementioned simplifications. In Figure 11, we compare the Dohnanyi (1969) and O'Brien & Greenberg (2003) steady-state mass distribution slope results with the ones given by our code at varying values of tensile strength slope. At s = 0 (constant Q*D), the O'Brien & Greenberg (2003) solution is equal to the traditional Dohnanyi (1969) value, but it gives steeper mass distribution slopes for lower values of s. Similar behavior is seen with our code; however, at s = 0 our prediction for the quasi-steady-state slope is ηm = 1.85 (ηa = 3.55), which is still steeper than the traditional value. At much lower values of s (< − 0.25) we predict a mass distribution slope that is less steep than the ones given by the O'Brien & Greenberg (2003) formula, while our results intersect at s = −0.25, yielding a quasi-steady-state slope of ηm = 1.87 (ηa = 3.61). Since the point of this intersection is close to the theoretical and experimental value of the tensile strength curve slope, the predictions from a pure steady-state model and a quasi-steady-state model will agree within errors. This renders the testing of different models difficult. However, our numerical calculations provide a general new estimate for the particle-size distribution slopes with significantly more complete physics compared to previous analytic approaches.

Figure 11.

Figure 11. Comparing the particle-mass distribution slope vs. tensile-strength curve slope of Dohnanyi (1969), O'Brien & Greenberg (2003), and our current work.

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5. SYNTHETIC SPECTRA

In the following sections, we compare the emission that results from the predicted particle-mass distributions to observations. As a first step, we generate an array of synthetic spectra using realistic astronomical silicate emission properties. We then analyze how the spectra are influenced by the particle-mass distribution function.

The flux emitted by a distribution of particle masses at a certain frequency is equal to

Equation (10)

where Qabs is the absorption efficiency coefficient, Bν(T) is the blackbody function, and ${\mathfrak v}$ is the total volume of the emitting region. Since in infrared astronomy it is customary to express the flux density as a function of wavelength, we rewrite this also as

Equation (11)

The exact function of the absorption efficiencies of particles in the interstellar medium or in circumstellar disks is largely unknown. The most commonly used particle types for SED calculations are artificial astronomical silicate (the properties of which are adjusted to reproduce the typical 10 μm silicate feature and measured laboratory dielectric functions) and graphite (Draine & Lee 1984). In Figure 12, we plot the absorption efficiency as a function of wavelength for a few astronomical silicate particle sizes. Particles larger than 10 μm have nearly constant absorption efficiency curves at shorter wavelengths (λ < 2πa, where a is the particle radius) with Qabs = 1, which is followed by a power-law cutoff. The slope of this power law becomes constant for wavelengths larger than ∼8πa and is commonly denoted by the variable β. Astronomical silicates of all sizes have a typical value of β = 2 (Draine & Lee 1984).

Figure 12.

Figure 12. Absorption efficiency of astronomical silicates as a function of wavelength for a range of particle sizes between 0.1 and 80 μm. Solid lines are the ∼λ−β approximations to the long-wavelength regimes of the curves that we employ in this work.

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In Figure 13, we show synthetic SEDs, all scaled to the same flux level at 1000 μm. The top panel shows spectra calculated around an A0 spectral-type star, with debris rings placed at various distances between 2 and 292 AU. The minimum particle-size cutoff was set at ∼5 μm, in accordance with our model (see Paper I). All disks with radial distances below ∼130 AU have a common slope for wavelengths larger than 250 μm, and the furthest disk at 292 AU joins this common slope around ∼350 μm.

Figure 13.

Figure 13. Synthetic SEDs for an array of model power-law particle-mass distributions, with varied parameters. The fluxes are scaled to match at 1000 μm. In the top panel, we show the synthetic SEDs generated for a variety of radial distances; in the middle panel, we show synthetic SEDs generated for a variety of minimum cutoffs (1, 2, 4, 8, 15, and 30 μm); and in the bottom panel, we show synthetic SEDs generated for a variety of particle-mass distribution slopes (1.80, 1.84, 1.88, 1.92, 1.96, and 1.99). Note that in the middle panel we vary the minimum cutoff of the particle-mass distributions, even though it is a parameter inherently set by equations in our collisional model. Since in reality, the placement of the cutoff is set by the optical properties and structural build of the micron-size particles, it is generally treated as a variable in SED models. In the plot, we show that such variations in the placement of the minimum cutoff do not affect the long-wavelength part of the SEDs.

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The blowout size in a system depends on grain structure (porosity) and the exact value of the optical constants for small grains (which is largely unknown and is a function of grain material). For this reason, we also calculated synthetic SEDs for a debris ring at 25 AU around an A0 spectral-type star, with the minimum particle size of the distribution artificially cutoff at sizes between 5 and 30 μm. (Note that we normally calculate the blowout mass self-consistently as described in Paper I.) We plot these SEDs in the middle panel of Figure 13. The offsets between the SEDs become apparent for wavelengths shorter than 200 μm, while for longer wavelengths, the emission profiles agree and have a common pseudo Rayleigh–Jeans slope.

Finally, we explore the dependence of the SED on the slope of the quasi-steady-state particle-mass distribution. The bottom panel of Figure 13 shows synthetic SEDs generated for a debris ring at 25 AU around an A0 spectral-type star, with a minimum particle cutoff size at 5 μm, but with particle-mass distribution slopes between 1.81 and 1.99. These plots show that the slope of the Rayleigh–Jeans part of the emission is greatly influenced by the particle-size distribution slope. In fact, it depends almost solely on this slope, with the temperature of the grains having mild effects at large orbital distances. We also performed our tests with dirty-ice optical constants (Preibisch et al. 1993) and found very similar results, showing that our results are also independent on particle types assumed.

6. RELATION BETWEEN THE PARTICLE-MASS DISTRIBUTION AND THE SED

The absorption efficiency curves can be simplified and described as

where x is a scaling constant for the power-law part of the function. Fitting the silicate absorption efficiency functions, we find

Equation (12)

Using this simplified absorption efficiency model and assuming that all particles contribute to the Rayleigh–Jeans tail of the SED with their own Rayleigh–Jeans emission, we estimate the emitted flux density at long wavelengths as

Equation (13)

Here, we assumed a β parameter that is independent of the particle size. The variable Cdisk is the number density scaling (see Paper I), kb is the Boltzmann constant, T is the temperature of the dust grains (which we also assume to be particle size independent), and D is the distance of the system from the observer. The quantity ηa is the quasi-steady-state particle-size distribution slope and can be calculated from the mass distribution slope as ηa = 3η − 2. Integrating these functions, we get

Equation (14)

where

Equation (15)

Equation (16)

Assuming β = 2, which is appropriate for astronomical silicates, we find that the slope of the SED is equal to −ηa for the short wavelength part of the Rayleigh–Jeans tail of the SED and 1 − ηa for the long-wavelength regime, where Qabs(λ, a) = 1 for the particles contributing the most to the emission. Similar results have been found by Wyatt & Dent (2002). This behavior explains why the slope of the flux density in the long-wavelength regime is not dependent on the optical properties of the grains, as Qabs(λ, a) = 1 for all grain types at these wavelengths that effectively contribute to it.

Our models yield a quasi-steady-state distribution slope of ηa ≈ 3.65, meaning that the Rayleigh–Jeans tail end of the SEDs should be proportional to

Equation (17)

as long as the particles are in collisional quasi-steady state.

7. COMPARISON TO OBSERVATIONS

To compare the computed spectra of quasi-steady-state collisional disks to data, we assembled the available data for debris disks with far-IR and submillimeter observations. As a result of our analysis in Section 5, where we determined the wavelength range that is least sensitive to parameters, we use only data at wavelengths larger than 250 μm. To fit a power law to the Rayleigh–Jeans regime of the SEDs, we need a minimum of three data points above our wavelength cutoff. We found a total of only nine sources that fulfill these requirements. We present the far-IR/submillimeter fluxes for these sources in Table 3. Occasionally, published submillimeter measurements do not account for systematic errors. In these cases, we applied a total of 30% error to all ground-based measurements at 350 and 450 μm and 15% for all Herschel data and measurements above 850 μm. We also made sure that the data included all the flux from each source and applied an aperture correction estimate otherwise. All corrections are listed as notes in Table 3.

Table 3. Observational Data of Debris Disks

Star λ Flux Error Excess Reference Notes
  (μm) (mJy) (mJy) (mJy)    
β Pic 250 1,900.0 285.0 1,897.5 Vandenbussche et al. (2010)  
  350 720.0 108.0 718.7 Vandenbussche et al. (2010)  
  500 380.0 57.0 379.4 Vandenbussche et al. (2010)  
  800 115.0 30.0 114.8 Zuckerman & Becklin (1993)  
  850 85.2 13.0 85.0 Holland et al. (1998)  
  850 104.3 16.0 103.8 Holland et al. (1998)  
  1200 24.3 4.0 24.2 Liseau et al. (2003)  
  1200 35.9 5.0 35.8 Liseau et al. (2003) Within 40''
  1300 24.9 4.0 24.8 Chini et al. (1991)  
epsilon Eri 350 366.0 109.8 359.45 Backman et al. (2009) CSO/SHARCII
  450 250.0 75.0 246.06 Greaves et al. (2005) JCMT/SCUBA
  850 37.0 5.55 35.92 Greaves et al. (2005) JCMT/SCUBA
  1300 24.2 4.0 23.74 Chini et al. (1991) JCMT/SCUBA
Fomalhaut 350 1,180.0 354.0 1,168.3 Marsh et al. (2005)  
  450 595.0 200.0 587.8 Holland et al. (2003)  
  850 97.0 14.55 95.1 Holland et al. (2003)  
  1300 21.0 3.5 20.17 Chini et al. (1991) Within 24''
  7000 0.4 0.065 0.37 Ricci et al. (2012)  
HD 8907 450 22.0 11.0 21.87 Najita & Williams (2005)  
  850 4.8 1.2 4.76 Najita & Williams (2005)  
  1200 3.2 0.9 3.18 Roccatagliata et al. (2009)  
HD 104860 350 50.1 15.0 50.0 Roccatagliata et al. (2009)  
  450 47.0 14.0 46.9 Najita & Williams (2005)  
  850 6.8 1.2 6.78 Najita & Williams (2005)  
  1200 4.4 1.1 4.39 Roccatagliata et al. (2009)  
  3000 1.35 0.67 1.35 Carpenter et al. (2005)  
HD 107146 350 319.0 90.0 318.8 Roccatagliata et al. (2009)  
  450 130.0 39.0 129.9 Najita & Williams (2005)  
  850 20.0 3.2 19.96 Najita & Williams (2005)  
  1300 10.4 3.0 10.39 Najita & Williams (2005)  
  3000 1.42 0.3 1.41 Carpenter et al. (2005)  
HR 8799 350 89.0 26.0 88.8 Patience et al. (2011)  
  850 15.0 3.0 14.96 Williams & Andrews (2006) Aperture correction
  1200 4.0 2.7 3.98 Bockelée-Morvan et al. (1994)  
Vega 250 1,680.0 260.0 1,617.6 Sibthorpe et al. (2010)  
  350 610.0 100.0 578.5 Sibthorpe et al. (2010)  
  500 210.0 40.0 194.8 Sibthorpe et al. (2010)  
  850 45.7 7.0 40.5 Holland et al. (1998)  
HD 207129 250 113.0 18.0 111.78 Marshall et al. (2011)  
  350 44.3 9.0 43.68 Marshall et al. (2011)  
  500 25.9 8.0 25.60 Marshall et al. (2011)  
  870 5.1 2.7 5.00 Nilsson et al. (2010)  

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We perform individual power-law fits to the data of each source as well as a fit to all sources simultaneously with a common Rayleigh–Jeans slope. In Figure 14, we present the photosphere subtracted excess emissions for each source in the left panels and plot the best-fit power-law spectrum of the form

Equation (18)

obtained from individual fits. We show in the right panels of Figure 14 the error contours of the slope and normalization of the power law at the 1σ, 2σ, and 3σ levels. The plots also indicate the χ2min/dof (the minimum of the reduced χ2) of each fit. The solid red line represents the Rayleigh–Jeans slope calculated from the Dohnanyi (1969) analytic solution, the green band represents the best slope given by our reference model calculation (including errors from 50% variations in the slope of the strength curve, see Figure 7), and the blue band yields our global-fit solution of

Equation (19)

The global fit and our reference model agree within the errors of the prediction.

Figure 14.
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Figure 14.

Figure 14. Observed SEDs of debris disks with submillimeter and millimeter data. The left panels are the photosphere-subtracted fluxes of the excess emissions with the best-fitting slopes, while the right panels are the 68%, 95%, and 99% confidence contours of the individual fits. The error contours also show the slope given by the Dohnanyi (1969) mass distribution function in red, the value predicted by our numerical code in the green band, and the best global fit with errors in the blue band.

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8. CONCLUSIONS

In this paper, we used our numerical model introduced in Paper I to follow the evolution of a distribution of particle masses. Our numerical model has been built to ensure mass conservation and that the resulting distribution of particles is not artificially offset due to numerical errors, as the integrations of the model span over 40 orders of magnitude in mass. In Section 2.4 of this paper, we demonstrate that lower precision integrations can lead to shallower particle distributions.

We varied all 12 collisional, all 6 system, and all 3 numerical variables of our model and examined the effects of these variations on the evolution of the particle-mass distribution. The quasi-steady-state particle distribution of the collisional system is extremely robust against variations in its variables, with the strongest effects occurring from changes to the tensile strength curve (Holsapple et al. 2002; Benz & Asphaug 1999). Even these variations have mild effects on the slope of the particle-mass distribution, modifying it only between the values of 1.84 and 1.94 (3.52 and 3.82 in size space, respectively). We find the dust-mass distribution of our reference model to be 1.88 (3.65 in size space). We find that waves occur when the collisional velocities are high or when particle strengths are low at the mass distribution cutoff, where the radiation force blowout dominates the dynamics. Nonetheless, in Section 3, we show that a simple power-law mass (size) distribution is an appropriate approximation even for extended disks with components only outside of 10–15 AU for solar- and 50–60 AU for early-type stars.

The Rayleigh–Jeans tail of the debris disk SEDs is dominated by the medium-sized particles, whose mass distribution is less affected by possible wavy structures. We derive a simple formula that gives the slope of the measured flux density in the Rayleigh–Jeans part of the SEDs as

This implies that the mass distribution slope itself could, in principle, be measured from long-wavelength observations. We assemble a list of nine debris disks that have been measured at the far-IR, submillimeter, and millimeter wavelengths and examine the Rayleigh–Jeans slope of their emissions. Our predictions of a slope of l = 2.65 ± 0.05 agrees well with the observations, which have a global slope fit of l = 2.58 ± 0.06.

Support for this work was provided by NASA through Contract No. 1255094 issued by JPL/Caltech. We thank Viktor Zubko and Karl Misselt for providing the numerical code to calculate the optical properties of large grains.

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10.1088/0004-637X/754/1/74