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ORDEM 4.0: NASA's Orbital Debris Engineering Model — A StatusFor over three decades, the NASA Orbital Debris Program Office (ODPO) has been developing the Orbital Debris Engineering Model (ORDEM) to provide satellite users and designers the resources necessary to compute collision risks from orbital debris. Iterations of this model compute information on the debris flux rates, direction, speed, size, and material densities based on the spacecraft asset’s orbit and predict the flux up to several decades in the future to encompass the time these spacecraft plan to operate. Engineering models need to be updated periodically as the environment and launch traffic changes (often in unpredictable ways). In addition, measurements, analysis techniques, and knowledge of the nature of orbital debris are constantly being improved, allowing the development of new capabilities.

The ORDEM 3 series are the most recent releases of the ORDEM model. They describe the debris flux in terms of material density of the debris in five categories: low-density (e.g., plastic), medium-density (e.g., aluminum), high-density (e.g., steel), intact objects, and the sodium-potassium (NaK) population. The material density is a significant parameter in determining which size debris will cause a given level of damage. Additionally, the outputs include an estimate of the uncertainties in the debris populations. The current version, ORDEM 3.2, was updated in 2022 to include the large debris cloud from the deliberate breakup of the Cosmos 1408 satellite on 15 November 2021.

This paper will describe the development and status of the newest ORDEM model, ORDEM 4.0. As with other ORDEM models, ORDEM 4.0 will include populations based on the most recent data from ground-based telescopes and radars as well as in situ measurements. The most important update, however, will be the inclusion of debris shapes, as this is another crucial parameter in determining how debris impacts damage surfaces. Extensive study of the recovered debris shapes from the DebriSat and prior experiments has allowed the ODPO to develop a simple model to parameterize the shapes as right circular cylinders. While this abstraction does not fully encompass all possible debris shape effects, these simplified shapes represent a major improvement in how damage is tested and computed. Further, a number of improved techniques have been introduced to model the debris populations; therefore, we will present the updated populations included in ORDEM 4.0 and how they compare to previous versions of ORDEM.
Document ID
20250002587
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Mark Matney
(Johnson Space Center Houston, United States)
Andrew Vavrin
(GeoControl Systems (United States) Houston, Texas, United States)
Michael Poehlmann
(Intuitive Machines Houston, Texas, United States)
Austen King
(Amentum Chantilly, Virginia, United States)
John H Seago
(Astrion (United States) Washington, United States)
Phillip Anz-Meador
(Amentum Chantilly, Virginia, United States)
Jer-Chyi Liou
(Johnson Space Center Houston, United States)
Corbin Cruz
(Amentum Chantilly, Virginia, United States)
Alyssa Manis
(Johnson Space Center Houston, United States)
Date Acquired
March 11, 2025
Subject Category
Space Transportation and Safety
Meeting Information
Meeting: 9th European Conference on Space Debris
Location: Bonn
Country: DE
Start Date: April 1, 2025
End Date: April 4, 2025
Sponsors: European Space Agency
Funding Number(s)
WBS: 817091.40.81.72
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Professional Review
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