2017
DOI: 10.1109/tps.2017.2711623
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Experimental Studies on Melt Erosion at Rail-Armature Contact of Rail Launcher in Current Range of 10–20 kA/mm

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Cited by 15 publications
(5 citation statements)
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“…For armature melting (as shown in Figure 6), Xia et al [38] used a payload-separation method to keep the recovered armatures intact. The experimental conditions included an armature and payload mass of 395.05 g, with a peak current ranging from 249.40 to 403.40 kA.…”
Section: Coupling Damagementioning
confidence: 99%
“…For armature melting (as shown in Figure 6), Xia et al [38] used a payload-separation method to keep the recovered armatures intact. The experimental conditions included an armature and payload mass of 395.05 g, with a peak current ranging from 249.40 to 403.40 kA.…”
Section: Coupling Damagementioning
confidence: 99%
“…The actual situation of current melting wave erosion in the armature is demonstrated by experimentally recovered armatures, where the actual process is more complex than predicted by the melting wave model [9][10][11][12]. Melting wave propagation is related to both the flow of the aluminum fluid and current distribution and is more obvious in stationary and low velocities situations.…”
Section: Armature Current Melting Wave Modelmentioning
confidence: 99%
“…[9]- [12]. As the deficit at L pr is associated with maximum rail current density [13], the transition is the main candidate for such a loss mechanism. The deficit at the acceleration has occurred at the late stage of the launch, which is a shred of strong evidence for transition.…”
Section: Introductionmentioning
confidence: 99%