We use Opik's analytical expressions that relate in a simple way the semimajor axis, eccentricity and inclination of the projectile orbit to the magnitude and direction of the relative velocity vector at impact on a given target on circular orbit, and the CODRM-94 model of debris population, to find that the large majority of the debris population is on orbits such that a correlation exists between their impact velocity on the ISS and the angle between the velocity vector of the impactor and that of the ISS.

A geometrical analysis of impacts on the ISS

Valsecchi GB;Rossi A
2001

Abstract

We use Opik's analytical expressions that relate in a simple way the semimajor axis, eccentricity and inclination of the projectile orbit to the magnitude and direction of the relative velocity vector at impact on a given target on circular orbit, and the CODRM-94 model of debris population, to find that the large majority of the debris population is on orbits such that a correlation exists between their impact velocity on the ISS and the angle between the velocity vector of the impactor and that of the ISS.
2001
Istituto di Scienza e Tecnologie dell'Informazione "Alessandro Faedo" - ISTI
Inglese
Proceedings of the third european conference on space debris
Third european conference on space debris
485
488
92-9092-733-X
Sì, ma tipo non specificato
19-21 marzo 2001
Darmstadt, Germania
Geometrical analysis
Codice PuMa: cnr.cnuce/2001-A2-017
2
reserved
Valsecchi, Gb; Rossi, A
273
info:eu-repo/semantics/conferenceObject
04 Contributo in convegno::04.01 Contributo in Atti di convegno
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/20.500.14243/113164
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