Improved performance of linear induction launchers

dc.contributor.authorBalikci, A
dc.contributor.authorZabar, Z
dc.contributor.authorBirenbaum, L
dc.contributor.authorCzarkowski, D
dc.date.accessioned2025-10-29T11:13:57Z
dc.date.issued2005
dc.departmentGebze Teknik Üniversitesi
dc.description12th Symposium on Electromagnetic Launch Technology -- MAY 25-28, 2004 -- Snowbird, UT
dc.description.abstractThis paper deals with the effect of parallel (rather than series) connection of the drive coils on the input voltage requirements, as well as on the energy utilization, of hypervelocity linear induction coil launchers fed by flywheel motor/generator sets. All of our previously published studies, 1987 to date, have dealt with series (rather than parallel) connected drive coils, which led to high input phase voltages and relatively low phase currents. In practice, the phase voltage per coil length should be kept below 30 kV/cm, the breakdown voltage of air. Furthermore, at any given time during the acceleration, the moving projectile (surrounded by a cylindrical sleeve) occupies only a portion of a barrel section length. When a parallel connection is used, the currents in the drive coils around the sleeve will be higher than the currents in the other coils in that section. That results in a greater accelerating force than in the series case, which leads to improved energy utilization. The simulation code used in our previously published work to predict the performance of a sectionalized, 3 kg projectile machine, was modified to obtain parallel-connection results for a similar machine. The paper describes the new drive-coil/pulse-generator configuration, explains the mathematical model, and provides graphs to compare the new results with those obtained previously with the series configuration.
dc.description.sponsorshipOff Naval Res Int Field Off,USA Res Lab
dc.identifier.doi10.1109/TMAG.2004.839283
dc.identifier.endpage175
dc.identifier.issn0018-9464
dc.identifier.issn1941-0069
dc.identifier.issue1
dc.identifier.orcid0000-0003-2621-1570
dc.identifier.scopus2-s2.0-12344330841
dc.identifier.scopusqualityQ2
dc.identifier.startpage171
dc.identifier.urihttps://doi.org/10.1109/TMAG.2004.839283
dc.identifier.urihttps://hdl.handle.net/20.500.14854/6996
dc.identifier.volume41
dc.identifier.wosWOS:000226342400005
dc.identifier.wosqualityQ2
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherIEEE-Inst Electrical Electronics Engineers Inc
dc.relation.ispartofIEEE Transactions on Magnetics
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.snmzKA_WOS_20251020
dc.subjectelectromagnetic launchers
dc.subjecthypervelocity launchers
dc.subjectinduction coil launchers
dc.titleImproved performance of linear induction launchers
dc.typeConference Object

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