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Predicting debrisThe probable amount, sizes, and relative velocities of debris are discussed, giving examples of the damage caused by debris, and focusing on the use of mathematical models to forecast the debris environment and solar activity now and in the future. Most debris are within 2,000 km of the earth's surface. The average velocity of spacecraft-debris collisions varies from 9 km/sec at 30 degrees of inclination to 13 km/sec near polar orbits. Mathematical models predict a 5 percent per year increase in the large-fragment population, producing a small-fragment population increase of 10 percent per year until the year 2060, the time of critical density. A 10 percent increase in the large population would cause the critical density to be reached around 2025.
Document ID
19880056290
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Kessler, Donald J.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 13, 2013
Publication Date
June 1, 1988
Publication Information
Publication: Aerospace America
Volume: 26
ISSN: 0740-722X
Subject Category
Astronautics (General)
Accession Number
88A43517
Distribution Limits
Public
Copyright
Other

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