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Exploring the Use of a Ground-Based Laser System to Deorbit Small Orbital Debris In March 2023, NASA Office of Technology, Policy, and Strategy (OTPS) released its Cost and Benefit Analysis of Orbital Debris Remediation report. This analysis found that the two most efficient methods for remediating orbital debris were the removal of small (1-10 cm) debris and nudging large debris away from predicted collisions; both methods could be performed by high-energy laser systems. To further explore the concept, OTPS has been assessing a reference mission using ground-based, pulsed lasers to detect, engage, and rapidly deorbit 1- to 10-cm debris that would otherwise threaten the safety of the International Space Station and future crewed platforms in low Earth orbit.

In March of 2024, OTPS convened a technical interchange meeting (TIM) of experts in detection and tracking of debris, high-energy glass and excimer lasers, laser-matter interactions, atmospheric propagation, and adaptive optics. The TIM spanned two days, covering the unclassified state of the art, uncertainties, and technical challenges for the entire concept of operations of the reference mission. In this presentation, we will summarize the reference mission analyzed, key findings from the TIM, and solicit the feedback from this community to further define “what is good enough” for debris remediation.
Document ID
20240005687
Acquisition Source
Headquarters
Document Type
Presentation
Authors
Thomas J. Colvin
(National Aeronautics and Space Administration Washington, United States)
Jericho Locke
(National Aeronautics and Space Administration Washington, United States)
Date Acquired
May 6, 2024
Subject Category
Lasers and Masers
Meeting Information
Meeting: Annual Directed Energy Science and Technology Symposium
Location: Colorado Springs, CO
Country: US
Start Date: May 20, 2024
End Date: May 24, 2024
Sponsors: Directed Energy Professional Society
Funding Number(s)
WBS: 10_398537.02.10_SSMX22024D
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Keywords
orbital debris
laser
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