The long evolution of the perigee altitude, above the nominal geostationary orbit, is studied under different GEO disposal orbit conditions. Diffent values of the disposal orbit altitude and eccentricity are considered. This presentation summarizes and compares the results of a set of orbital propagations, of commonly agreed test cases, between the following Space Agencies: ASI, BNSC, CNSA, ESA, ISRO and NASA.

AI 22.1 - GEO disposal orbit eccentricity

Rossi A;
2006

Abstract

The long evolution of the perigee altitude, above the nominal geostationary orbit, is studied under different GEO disposal orbit conditions. Diffent values of the disposal orbit altitude and eccentricity are considered. This presentation summarizes and compares the results of a set of orbital propagations, of commonly agreed test cases, between the following Space Agencies: ASI, BNSC, CNSA, ESA, ISRO and NASA.
2006
Istituto di Scienza e Tecnologie dell'Informazione "Alessandro Faedo" - ISTI
J.2 Physical Science and Engineering
Space debris
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/20.500.14243/102151
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