2015
DOI: 10.1017/s0022377815000318
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Cylindrical liner Z-pinch experiments for fusion research and high-energy-density physics

Abstract: A gas-filled cylindrical liner z-pinch configuration has been used to drive convergent radiative shock waves into different gases at velocities of 20–50 km s−1. On application of the 1.4 MA, 240 ns rise-time current pulse produced by the Magpie generator at Imperial College London, a series of cylindrically convergent shock waves are sequentially launched into the gas-fill from the inner wall of the liner. This occurs without any bulk motion of the liner wall itself. The timing and trajectories of the shocks a… Show more

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Cited by 16 publications
(13 citation statements)
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“…This yielded a launch time of 187 ± 24 ns after the current start. These launch times are comparable to those seen in previous converging shock experiments [24] while velocities are slower by a factor of 2 (∼10 km/s instead of ∼20 km/s) primarily due to the increased mass density of the gas-fill. However, in contrast to the multiple shocks observed in converging shock experiments, only a single shock (ignoring edge effects) is observed in the experiments described in this paper.…”
Section: A Optical Self-emissionsupporting
confidence: 84%
See 1 more Smart Citation
“…This yielded a launch time of 187 ± 24 ns after the current start. These launch times are comparable to those seen in previous converging shock experiments [24] while velocities are slower by a factor of 2 (∼10 km/s instead of ∼20 km/s) primarily due to the increased mass density of the gas-fill. However, in contrast to the multiple shocks observed in converging shock experiments, only a single shock (ignoring edge effects) is observed in the experiments described in this paper.…”
Section: A Optical Self-emissionsupporting
confidence: 84%
“…It is possible to produce radiative shocks in laboratory experiments using lasers focused onto a pin embedded in a gas [9], a cluster gas [10]- [12], or a piston attached to a gas cell [13]- [21]. Radiative shocks have also been produced on pulsed power generators using imploding liners with an internal gas fill [22]- [24]. In these experiments, ∼1 MA of current was discharged through a gas-filled liner (a thin-walled metal tube).…”
Section: Introductionmentioning
confidence: 99%
“…The fitting of the RPL and these proposed criteria have been already used to predict the possibility of thermal instabilities in experiments of convergent radiative shocks in argon and neon produced in a cylindrical liner Z-pinch configuration [24] and also in experiments of blast waves launched in clusters of xenon [17,26,60]. In both cases, the results obtained theoretically were consistent with the experimental observations.…”
Section: Analysis Of Thermal Instabilities In the Bow Shocksupporting
confidence: 57%
“…The first one is the analysis of the validity of LTE assumption in the calculation of average microscopic properties of argon plasmas in mass densities and electron temperatures ranging from 10 −6 to 10 −1 g cm −3 and from 1 to 100 eV, respectively. Argon is an element commonly used in laboratory astrophysics experiments on radiative shocks generated using either pulsed power devices [19,[21][22][23][24] or ultraintense lasers [17,[25][26][27][28][29][30], and the ranges of plasma conditions of these experiments fall within the ones before mentioned, hence, the interest of this study. For this analysis, we have made calculations assuming the plasma either in LTE and therefore using the Saha-Boltzmann (SB) equations, or in non-LTE (NLTE) in steady state, in which we have solved the rate equations implemented in our collisional-radiative model.…”
Section: Introductionmentioning
confidence: 99%
“…We have already used our fitting of the RPL and these criteria to predict the possibility of isobaric radiative cooling instabilities experiments of convergent radiative shocks in argon and neon generated in a cylindrical liner Z-pinch configuration, obtaining results that are consistent with the experimental observations [71].…”
Section: E Thermal Instabilities In the Cooling Layermentioning
confidence: 55%