{"title":"Advances in Electromagnetic Launch Science and Technology and its Applications","authors":"H. Fair","doi":"10.1109/elt.2008.9","DOIUrl":"https://doi.org/10.1109/elt.2008.9","url":null,"abstract":"The US continues a broad spectrum of research to provide the scientific underpinnings for electromagnetic launch. These efforts include fundamental research on materials, properties of materials subjected to electromagnetic and thermal stress, railguns (particularly the rail-armature sliding interface), coilguns and energy storage and power conditioning. There is also broad and growing interest in novel applications of electromagnetic launch. For example, a supersonic beam of neon atoms have been slowed and stopped opening the door to investigating the atomic and molecular properties of most of the periodic table of atoms and certain molecules. Research is continuing on magnetic brakes, and the more traditional research on the launch of materials to hypervelocities. More recently, the launching of materials into earth's orbit or even deeper in space is obtaining renewed interest. Consequently, some attention is being given to the types of materials of projectiles for hypersonic flight. The US Navy has initiated new multidisciplinary University Research teams including physics, chemistry, and materials science to develop new diagnostic tools and to provide a more detailed examination of the rail-armature interface. Most significantly, the US Army has elevated its emphasis from electromagnetic launch science and technology development to the operational consequences of long-range precision fires. In concert with the recent US Navy efforts on long-range fires, it is anticipated that the pull of these applications will enable even greater advances in the science and technology of electromagnetic launch.","PeriodicalId":170049,"journal":{"name":"2008 14th Symposium on Electromagnetic Launch Technology","volume":"59 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114059756","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"Integral Formulation of the Problem of Current Distribution in Compulsator Wires of Electromagnetic Launchers and Railguns","authors":"K. Sheshadri","doi":"10.1109/elt.2008.105","DOIUrl":"https://doi.org/10.1109/elt.2008.105","url":null,"abstract":"Compulsators are power sources of choice for use in electromagnetic launchers and railguns. These devices hold the promise of reducing unit costs of payload to orbit. In earlier work the author had calculated the current distribution in compulsator wires by considering the wire to be split into a finite number of separate wires. The present work develops an integral formulation of the problem of current distribution in compulsator wires which leads to an integro-differential equation. Analytical solutions including for the integration constants are obtained in closed form. The analytical solutions present a much clearer picture of the effect of various input parameters on the cross sectional current distribution and point to ways in which desired current density distribution can be achieved. Results are graphically presented and discussed with particular reference to a 50 kJ compulsator in Bangalore. Finite element analysis supports the results.","PeriodicalId":170049,"journal":{"name":"2008 14th Symposium on Electromagnetic Launch Technology","volume":"40 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"129746912","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"Thermal Stresses Analysis of the Rails and the Armature of an Electromagnetic Launcher","authors":"M. Ghassemi, M. Varmazyar","doi":"10.1109/elt.2008.92","DOIUrl":"https://doi.org/10.1109/elt.2008.92","url":null,"abstract":"In an electromagnetic launcher, the magnetic field creates a dynamic force that moves the armature forward. During the launch, electrical current creates high body forces and temperature distribution in the rails and the armature. As a result the rails and armature experience high amplitude stress and strain which damage the rails and the armature and reduces their life span. The purpose of this paper is to investigate the effect of body force as well as the temperature distribution on the displacement of the rails in an electromagnetic launcher. In this study the physical and geometrical properties of the rails are constant in location. In our formulation of governing non-linear differential equations, Maxwell, Energy equation and Navier equation are applied to the rails under dynamic loading. To solve the non-linear governing differential equations a finite difference base code is developed and utilized. It is shown that the Maximum volumetric forces take place where the highest magnetic field gradient occurs. In addition, the maximum magnetic force is accumulated at the trailing edge of the armature and portions of the rail interior. The thermal stresses distribution follows the same trend as displacement due to temperature behavior of the rails.","PeriodicalId":170049,"journal":{"name":"2008 14th Symposium on Electromagnetic Launch Technology","volume":"110 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"117251467","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
E. Spahn, K. Sterzelmeier, C. Gauthier-Blum, V. Brommer, L. Sinniger, B. Grasser
{"title":"50 kJ Ultra-Compact Pulsed-Power Supply Unit for Active Protection Launcher Systems","authors":"E. Spahn, K. Sterzelmeier, C. Gauthier-Blum, V. Brommer, L. Sinniger, B. Grasser","doi":"10.1109/elt.2008.13","DOIUrl":"https://doi.org/10.1109/elt.2008.13","url":null,"abstract":"The impulsive acceleration of active protection elements such as armour plates or other terminal ballistics interception devices can preferably be realized by single-stage electromagnetic launcher systems using pancake coils. The technology with controlled multipartite coil assemblies represents a new supplementary topic in the entire field of ballistics. But the essential condition is the availability of modular high energy density pulsed power supply units with low volume and weight. During the last years modular structured energy packs have been built up at ISL as a basic installation for various applications in the field of pulsed power electronics, in particular they are developed to feed active protection launcher systems. Each power supply module comprises one energy storage capacitor, a thyristor stack, a corresponding number of crow-bar diodes and a well-designed coaxial power line serving as a pulse forming network and current limiting reactor. To provide high flexibility these modules can be triggered separately and independently by fiber optic transmitters with an overall jitter lower than 50 ns. The paper presented describes the basic design of a 50 kJ energy pack and the further developed set-up with a strongly reduced overall height obtained by using a novel multichip thyristor. Additionally a two dimensional steerable launcher system supplied by these modules will be presented.","PeriodicalId":170049,"journal":{"name":"2008 14th Symposium on Electromagnetic Launch Technology","volume":"165 3","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114100235","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"Two-Objective Optimization Design for Pulsed Power Supply","authors":"Zhengjun Shi, Xinjie Yu","doi":"10.1109/elt.2008.94","DOIUrl":"https://doi.org/10.1109/elt.2008.94","url":null,"abstract":"A novel two-objective optimization design model for pulsed power supply (PPS) is proposed in this paper. The objectives are the muzzle velocity and the stored-to-kinetic energy efficiency. The design variables include the operating voltage and the trigger delay times between segments. The acceleration of the armature is constrained to lower than 106 m/s2. The optimization results for the muzzle velocity and the efficiency separately show that (1) the acceleration constraint has great influence on the performance; (2) wide current pulse yields high velocity but low efficiency; and (3) the operating voltage has to be increased to accelerate a heavier projectile to a certain velocity, or at a certain efficiency. Pareto solution fronts for various projectile masses are found using the non-dominated sorting genetic algorithm (NSGA-II) under the integration environment of iSIGHTTM software. Numerical results show that the NSGA-II can provide a set of feasible Pareto solutions for the two-objective optimization design model of PPS, among which the \"best\" one is to be extracted according to the designer's requirements.","PeriodicalId":170049,"journal":{"name":"2008 14th Symposium on Electromagnetic Launch Technology","volume":"41 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"127443552","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
D. Motes, J. Ellzey, S. Levinson, J. Parker, F. Stefani, D. Wetz
{"title":"A Study of Electrothermal Launcher Efficiencies and Gas Dynamics","authors":"D. Motes, J. Ellzey, S. Levinson, J. Parker, F. Stefani, D. Wetz","doi":"10.1109/elt.2008.114","DOIUrl":"https://doi.org/10.1109/elt.2008.114","url":null,"abstract":"This paper describes a series of experiments to study the efficiency of an electrothermal (ET) launcher. The launcher serves as a pre-accelerator for a plasma-driven hypervelocity railgun experiment at the Institute for Advanced Technology. The ET launcher is designed to accelerate small polycarbonate projectiles to about 1 km/s. The objective of this study was to understand how pulse duration affects the efficiency with which the pressure of the ET discharge is coupled to the projectile. The study consisted of multiple tests for which the total energy of the discharge was kept constant, but the pulse length was varied. The dependent variable in the tests was the muzzle velocity of the projectile. The experimental results are presented and compared with gas-dynamic considerations.","PeriodicalId":170049,"journal":{"name":"2008 14th Symposium on Electromagnetic Launch Technology","volume":"31 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"128354077","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"The Use of Electronic Components in Railgun Projectiles","authors":"R. Ciolini, M. Schneider, B. Tellini","doi":"10.1109/elt.2008.124","DOIUrl":"https://doi.org/10.1109/elt.2008.124","url":null,"abstract":"This paper deals with experiments and calculations performed in order to investigate the influence of the electromagnetic hardening of payloads in a railgun. This is a complex task: besides the large amplitudes of the in-bore magnetic fields due to the pulsed current, the exit of the projectile from the muzzle and the consequences of plasma arcs have to be considered. At the muzzle the magnetic induction can drop from several Teslas to zero within some microseconds, leading to very high induced voltages and electric fields in the metallic parts of the projectile. On the other hand, the electric contact established by solid armatures tends to develop into electric arcs at high velocities during the launch. These plasma arcs as well as the closing switch transients of the railgun circuit are a source of electromagnetic radiation in a broad spectral range. Some electronic devices were selected and tested with static setups corresponding to the previous conditions. In a first phase a series of static railgun experiments (no projectile movement) was performed. In a second phase, static experiments simulating the muzzle exit conditions were carried out. Finally, the influence of electromagnetic waves emitted during railgun experiments on electronic devices was investigated, using a static setup with a conventional spark gap.","PeriodicalId":170049,"journal":{"name":"2008 14th Symposium on Electromagnetic Launch Technology","volume":"8 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"126015356","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"Melting and Cavity Growth in the Vicinity of Crack Tips Subjected to Short-Duration Current Pulses","authors":"F. Gallo, S. Satapathy, K. Ravi-Chandar","doi":"10.1109/elt.2008.121","DOIUrl":"https://doi.org/10.1109/elt.2008.121","url":null,"abstract":"The current-carrying conductors in an electromagnetic launcher are exposed to high currents that last for a few milliseconds. Surface cracks on the rails can generate large gradients in current in their vicinity and may result, in some instances, in localized melting and expulsion of rail material. Here, we report the results of a study in which the mechanical and electrical parameters of the process were monitored as a function of time and the evolution of melting and ejection was examined through high-speed photography.","PeriodicalId":170049,"journal":{"name":"2008 14th Symposium on Electromagnetic Launch Technology","volume":"15 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"121484439","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"Effect of Magnetic Flux Density and Other Properties on Temperature and Velocity Distribution in Magnetohydrodynamic Pump (MHD)","authors":"M. Ghassemi, A. Shahidian","doi":"10.1109/elt.2008.32","DOIUrl":"https://doi.org/10.1109/elt.2008.32","url":null,"abstract":"The interaction of moving conducting fluids with electric and magnetic fields provides the magnetohydrodynamic (MHD) phenomenon. Based on this principle, MHD pump uses the \"Lorentz force\" to move fluid. The railgun channel is one important segment in an electromagnetic launcher. As known one of the possible ways to increase the EML efficiency is to segment the working channel. For this purpose MHD flow study is necessary. It is required to have the knowledge of the flow field and the temperature to design a magnetohydrodynamic pump. The purpose of this study is to investigate the effect of the magnetic flux density and current on the flow and the temperature distribution in a magnetohydrodynamic pump. To solve the governing differential equations, a finite difference based code is developed and utilized. The temperature and velocity are calculated by solving the energy and the Navier-Stokes equations. Results show a maximum value of velocity for different values of magnetic flux density (B). However the temperature stays almost constant with magnetic field. In addition as current increases, the velocity and the temperature increase too.","PeriodicalId":170049,"journal":{"name":"2008 14th Symposium on Electromagnetic Launch Technology","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"131202447","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"Inductive Pulsed-Power Supply with Marx Generator Methodology","authors":"Y. Aso, T. Hashimoto, T. Abe, S. Yamada","doi":"10.1109/elt.2008.50","DOIUrl":"https://doi.org/10.1109/elt.2008.50","url":null,"abstract":"We have been developing an inductive pulsed-power supply consisting of many coils with Marx generator methodology. A Marx generator is charged in a parallel connection of capacitors and discharged in a series connection to obtain a high-voltage impulse. In contrast, this inductive pulsed- power supply is excited in a series connection of coils and discharged in the parallel connection to obtain a pulsed large electric current. Our preliminary experiment showed that this process was correct. As the next step, we have developed a prototype of the inductive pulsed-power supply, which we call the current multiplier by inductive storage (CMIS). Here we describe the CMIS characteristics and the results of experiments using CMIS.","PeriodicalId":170049,"journal":{"name":"2008 14th Symposium on Electromagnetic Launch Technology","volume":"119 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"127561101","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}