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Orbital Debris MitigationPolicies on limiting orbital debris are found throughout the US Government, many foreign space agencies, and as adopted guidelines in the United Nations. The underlying purpose of these policies is to ensure the environment remains safe for the operation of robotic and human spacecraft in near‐ Earth orbit. For this reason, it is important to consider orbital debris mitigation during the design of all space vehicles. Documenting compliance with the debris mitigation guidelines occurs after the vehicle has already been designed and fabricated for many CubeSats, whereas larger satellites are evaluated throughout the design process. This paper will provide a brief explanation of the US Government Orbital Debris Mitigation Standard Practices, a discussion of international guidelines, as well as NASA's process for compliance evaluation. In addition, it will discuss the educational value of considering orbital debris mitigation requirements as a part of student built satellite design.
Document ID
20140003405
Acquisition Source
Johnson Space Center
Document Type
Abstract
Authors
Kelley, R. L.
(Jacobs Technology, Inc. Houston, TX, United States)
Jarkey, D. R.
(Jacobs Technologies Engineering Science Contract Group Houston, TX, United States)
Stansbery, G.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
April 23, 2014
Publication Date
January 1, 2014
Subject Category
Space Sciences (General)
Spacecraft Design, Testing And Performance
Report/Patent Number
JSC-CN-30842
Report Number: JSC-CN-30842
Meeting Information
Meeting: Annual Cubesat Developers Conference
Location: San Luis Obispo, CA
Country: United States
Start Date: April 23, 2014
End Date: April 25, 2014
Distribution Limits
Public
Copyright
Public Use Permitted.
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