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Satellite disintegration dynamicsThe subject of satellite disintegration is examined in detail. Elements of the orbits of individual fragments, determined by DOD space surveillance systems, are used to accurately predict the time and place of fragmentation. Dual time independent and time dependent analyses are performed for simulated and real breakups. Methods of statistical mechanics are used to study the evolution of the fragment clouds. The fragments are treated as an ensemble of non-interacting particles. A solution of Liouville's equation is obtained which enables the spatial density to be calculated as a function of position, time and initial velocity distribution.
Document ID
19760028358
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dasenbrock, R. R.
(Naval Research Lab. Washington, DC, United States)
Kaufman, B.
(Naval Research Lab. Washington, DC, United States)
Heard, W. B.
(U.S. Navy, Naval Research Laboratory, Washington D.C., United States)
Date Acquired
August 8, 2013
Publication Date
July 1, 1975
Subject Category
Astrodynamics
Report/Patent Number
AAS PAPER 75-040
Meeting Information
Meeting: Astrodynamics Specialist Conference
Location: Nassau
Country: Bahamas
Start Date: July 28, 1975
End Date: July 30, 1975
Sponsors: American Astronautical Society and American Institute of Aeronautics and Astronautics
Accession Number
76A11324
Funding Number(s)
CONTRACT_GRANT: NASA ORDER L-5106-A
Distribution Limits
Public
Copyright
Other

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