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Spacecraft launching technique and systems

dc.contributor.authorIlcev, Stojce Dimov
dc.date.accessioned2018-05-29T06:39:03Z
dc.date.available2018-05-29T06:39:03Z
dc.date.issued2016
dc.description.abstractIn this paper is presented the spacecraft launching technique and different rocket systems. The launch of the satellite and controlling support services are a very critical point in the creation of space-based communication technology and the most expensive phase of the total system cost. At the same time, the need to make a satellite body capable of surviving the stresses of the launch stages is a major element in their design phase. Satellites are also designed to be compatible with more then one model of launch vehicle and launching type. In a more determined sense, the multi-stage expendable and manned or unmanned reusable launchers are described. Owing to location and type of site here are discussed land-based and sea-based launch systems. The new sea launch multinational system was developed more than ten years ago to overcome the cost of land-based launch infrastructure duplication around the world. Additional rocket motors during launching procedure, such as perigee and apogee kick propulsion systems, may also be required.en_US
dc.dut-rims.pubnumDUT-005840en_US
dc.format.extent4 pen_US
dc.identifier.citationIlcev. S.D. 2016. Spacecraft launching technique and systems. International Conference on Electrical, Electronics, and Optimization Techniques (ICEEOT) - 2016. 4514-4517.en_US
dc.identifier.issn978-1-4673-9939-5 (e)
dc.identifier.urihttp://hdl.handle.net/10321/2999
dc.language.isoenen_US
dc.publisherIEEEen_US
dc.publisher.urihttps://ieeexplore.ieee.org/stamp/stamp.jsp?tp=&arnumber=7755572en_US
dc.relation.ispartofSouth African journal of sports medicine (Online)
dc.subjectGEOen_US
dc.subjectSatellite Launcheren_US
dc.subjectHohmann Transfer Ellipseen_US
dc.subjectSatellite Orbiten_US
dc.subjectLaunching Vehiclesen_US
dc.titleSpacecraft launching technique and systemsen_US
dc.typePresentationen_US
local.sdgSDG17

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