The two-body problem with drag and radiation pressure

Mavraganis, AG; Michalakis, DG

dc.contributor.author	Mavraganis, AG	en
dc.contributor.author	Michalakis, DG	en
dc.date.accessioned	2014-03-01T01:10:20Z
dc.date.available	2014-03-01T01:10:20Z
dc.date.issued	1994	en
dc.identifier.issn	0923-2958	en
dc.identifier.uri	https://dspace.lib.ntua.gr/xmlui/handle/123456789/11370
dc.subject	atmospheric drag	en
dc.subject	Radiation pressure	en
dc.subject.classification	Astronomy & Astrophysics	en
dc.subject.classification	Mathematics, Interdisciplinary Applications	en
dc.title	The two-body problem with drag and radiation pressure	en
heal.type	journalArticle	en
heal.identifier.primary	10.1007/BF00692013	en
heal.identifier.secondary	http://dx.doi.org/10.1007/BF00692013	en
heal.language	English	en
heal.publicationDate	1994	en
heal.abstract	The Kepler problem including radiation pressure and drag is treated. The equation of the orbit is derived and the scalar and vector integrals of motion are obtained by direct operation on the vector form of the equation of motion. © 1994 Kluwer Academic Publishers.	en
heal.publisher	Kluwer Academic Publishers	en
heal.journalName	Celestial Mechanics & Dynamical Astronomy	en
dc.identifier.doi	10.1007/BF00692013	en
dc.identifier.isi	ISI:A1994ND98200007	en
dc.identifier.volume	58	en
dc.identifier.issue	4	en
dc.identifier.spage	393	en
dc.identifier.epage	403	en