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- W3116243281 abstract "This paper describes the general procedures and resources required for a determination of specific orbits of space debris resulting from satellite breakups and other causes. The initial coincidence of all pieces combined with the limited discrimination ability of tracking radars causes confusion in this process. The Naval Space Surveillance Center uses a technique called blast-point analysis to analyze the orbits of specific debris pieces as rapidly as possible. The details of this procedure are described, together with practical factors involved in actual breakup events. Evidence of fragment behavior is presented from the breakups of COSMOS 1823, TIROS N, and two other COSMOS satellites. Typical numbers of trackable pieces are 100-300. Typical fragment relative velocities range from 5 to 125 m/s, with an average value near 50 m/s. Evidence is presented to confirm the generally accepted model of near-term debris behavior that shows a secular dispersion in the along-track direction, with more strictly cyclical behavior in the cross-track component." @default.
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- W3116243281 date "1990-04-01" @default.
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- W3116243281 title "Orbital elements determination for breakup and debris" @default.
- W3116243281 hasPublicationYear "1990" @default.
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