Pulsed Laser Interactions with Space Debris: Target Shape Effects
D. A. Liedahl, A. Rubenchik, S. B. Libby, S. Nikolaev, and C. R., Phipps

TL;DR
This paper investigates how the shape of space debris affects recoil dynamics during laser ablation for de-orbiting, developing analytical models to predict momentum transfer and spin changes, which are crucial for effective debris mitigation.
Contribution
It introduces a simple analytical technique to calculate shape-dependent recoil and spin effects during laser ablation of space debris, enhancing predictive capabilities for debris removal strategies.
Findings
Shape and orientation significantly influence recoil direction and magnitude.
Ablation can alter the spin state of debris targets.
Shape effects on momentum transfer are similar to, but distinct from, photon pressure effects.
Abstract
Among the approaches to the proposed mitigation and remediation of the space debris problem is the de-orbiting of objects in low Earth orbit through irradiation by ground-based high-intensity pulsed lasers. Laser ablation of a thin surface layer causes target recoil, resulting in the depletion of orbital angular momentum and accelerated atmospheric re-entry. However, both the magnitude and direction of the recoil are shape dependent, a feature of the laser-based remediation concept that has received little attention. Since the development of a predictive capability is desirable, we have investigated the dynamical response to ablation of objects comprising a variety of shapes. We derive and demonstrate a simple analytical technique for calculating the ablation-driven transfer of linear momentum, emphasizing cases for which the recoil is not exclusively parallel to the incident beam. For…
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