IEEE Transactions on Magnetics · 1991 · 15 citations · 3 references
EngineeringAerospace EngineeringAerospace StructuresPlasma PhysicsSpacecraft DesignAccelerator PhysicsSpacecraft StructuresElectromagnetic Launch SystemsEnergy Efficiency DiagnosticsLaunch PerformanceLaunchersProjectile KineticsProjectile Technology
A small-scale, 10-stage cylindrical reconnection launcher has been designed, fabricated, and tested. Ten-gram projectiles are accelerated from rest to 317 m/s through the 0.44-m launcher assembly with a projectile kinetic energy to capacitor stored energy efficiency of 9%. Comparison of test results and computer code predictions are presented. Results of these studies have substantiated launcher scaling at small size and have provided a useful test bed for launcher components and diagnostics.< <ETX xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink">></ETX>
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Exploratory development of the reconnection launcher 1986-90
M. Cowan, M. M. Widner, E.C. Cnare et al. · IEEE Transactions on Magnetics · 1991 · 33 citations
Engineering, Aerospace Engineering, Electrical Engineering +12