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The Cost of Future Collisions in LEO - Star Technology and Research

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30<br />

To put estimate (B5) <strong>in</strong> perspective, let us consider a commonly used formula<br />

N m = k (M/m) γ ,<br />

(B6)<br />

where N m is the number <strong>of</strong> fragments heavier than m, <strong>and</strong> M is the total mass <strong>in</strong>volved<br />

<strong>in</strong> the collision. <strong>The</strong> orig<strong>in</strong>al Kessler’s formula has k ≈ 0.8 <strong>and</strong> γ ≈ 0.8 [21],<br />

an early version <strong>of</strong> the NASA breakup model uses k ≈ 0.45 <strong>and</strong> γ ≈ 0.75 [18], the<br />

mass distribution <strong>of</strong> the tracked fragments <strong>of</strong> Solw<strong>in</strong>d fits k ≈ 0.3 <strong>and</strong> γ ≈ 0.8 [16],<br />

while the estimate (B5) corresponds to k ≈ 0.4 <strong>and</strong> γ ≈ 0.8 for M ∼ 1 ton. Extended<br />

formally toward masses over 10 kg, the estimated distribution converges<br />

with the early NASA model. Debris models are evolv<strong>in</strong>g [22], <strong>and</strong> new breakup<br />

models are <strong>in</strong>troduced [20, 23]. <strong>The</strong>y will become more accurate when more data<br />

on small fragments is gathered.

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