Analyze of multistage transfer orbit to reach the GEO orbit in a rotational symmetric gravitational field

Simple item page
dc.creatorNg, S.
dc.date2005-11-13
dc.date.accessioned2026-07-07T06:52:19Z
dc.date.available2026-07-07T06:52:19Z
dc.descriptionPlacing satellites in geostationary obital (GEO) is propellant exigeant. It requires large propellant consumption that will take a large part of the total mass. Hence the interest is reduce the mass of propellant loaded both in the rocket and the satellite. Both for improving selection of transfer orbits and propellant. In this paper we give a reiew of analysis of launching of satellite to GEO using multistage transfer orbit in order to reduce the mass of propellant. Making this analysis complete, the effect of the general relativity regarding elliptical transfer orbit and its potensial utilization will be briefly reviewed.
dc.description13 pages
dc.identifierhttps://arxiv.org/abs/physics/0511114
dc.identifierhttp://arxiv.org/abs/physics/0511114
dc.identifier.urihttp://salesiana.dossiersoluciones.com/handle/123456789/105265
dc.subjectSpace Physics
dc.titleAnalyze of multistage transfer orbit to reach the GEO orbit in a rotational symmetric gravitational field
dc.typetext

Files

Collections

arXiv