B. K. Spears
Lawrence Livermore National Laboratory
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Physics of Plasmas | 2011
S. W. Haan; J. D. Lindl; D. A. Callahan; D. S. Clark; J. D. Salmonson; B. A. Hammel; L. J. Atherton; R. Cook; M. J. Edwards; S. H. Glenzer; Alex V. Hamza; S. P. Hatchett; Mark Herrmann; D. E. Hinkel; D. Ho; H. Huang; O. S. Jones; J. L. Kline; G. A. Kyrala; O. L. Landen; B. J. MacGowan; M. M. Marinak; D. D. Meyerhofer; J. L. Milovich; K. A. Moreno; E. I. Moses; David H. Munro; A. Nikroo; R. E. Olson; Kyle Peterson
Point design targets have been specified for the initial ignition campaign on the National Ignition Facility [G. H. Miller, E. I. Moses, and C. R. Wuest, Opt. Eng. 443, 2841 (2004)]. The targets contain D-T fusion fuel in an ablator of either CH with Ge doping, or Be with Cu. These shells are imploded in a U or Au hohlraum with a peak radiation temperature set between 270 and 300 eV. Considerations determining the point design include laser-plasma interactions, hydrodynamic instabilities, laser operations, and target fabrication. Simulations were used to evaluate choices, and to define requirements and specifications. Simulation techniques and their experimental validation are summarized. Simulations were used to estimate the sensitivity of target performance to uncertainties and variations in experimental conditions. A formalism is described that evaluates margin for ignition, summarized in a parameter the Ignition Threshold Factor (ITF). Uncertainty and shot-to-shot variability in ITF are evaluated, and...
Physics of Plasmas | 2011
M. J. Edwards; J. D. Lindl; B. K. Spears; S. V. Weber; L. J. Atherton; D. L. Bleuel; David K. Bradley; D. A. Callahan; Charles Cerjan; D. S. Clark; G. W. Collins; J. Fair; R. J. Fortner; S. H. Glenzer; S. W. Haan; B. A. Hammel; Alex V. Hamza; S. P. Hatchett; N. Izumi; B. Jacoby; O. S. Jones; J. A. Koch; B. J. Kozioziemski; O. L. Landen; R. A. Lerche; B. J. MacGowan; A. J. Mackinnon; E. R. Mapoles; M. M. Marinak; M. J. Moran
Ignition requires precisely controlled, high convergence implosions to assemble a dense shell of deuterium-tritium (DT) fuel with ρR>∼1 g/cm2 surrounding a 10 keV hot spot with ρR ∼ 0.3 g/cm2. A working definition of ignition has been a yield of ∼1 MJ. At this yield the α-particle energy deposited in the fuel would have been ∼200 kJ, which is already ∼10 × more than the kinetic energy of a typical implosion. The National Ignition Campaign includes low yield implosions with dudded fuel layers to study and optimize the hydrodynamic assembly of the fuel in a diagnostics rich environment. The fuel is a mixture of tritium-hydrogen-deuterium (THD) with a density equivalent to DT. The fraction of D can be adjusted to control the neutron yield. Yields of ∼1014−15 14 MeV (primary) neutrons are adequate to diagnose the hot spot as well as the dense fuel properties via down scattering of the primary neutrons. X-ray imaging diagnostics can function in this low yield environment providing additional information about ...
Physics of Plasmas | 2011
O. L. Landen; John Edwards; S. W. Haan; H. F. Robey; J. L. Milovich; B. K. Spears; S. V. Weber; D. S. Clark; J. D. Lindl; B. J. MacGowan; E. I. Moses; J. Atherton; Peter A. Amendt; T. R. Boehly; David K. Bradley; David G. Braun; D. A. Callahan; Peter M. Celliers; G. W. Collins; E. L. Dewald; L. Divol; J. A. Frenje; S. H. Glenzer; Alex V. Hamza; B. A. Hammel; D. G. Hicks; Nelson M. Hoffman; N. Izumi; O. S. Jones; J. D. Kilkenny
Capsule performance optimization campaigns will be conducted at the National Ignition Facility [G. H. Miller, E. I. Moses, and C. R. Wuest, Nucl. Fusion 44, 228 (2004)] to substantially increase the probability of ignition. The campaigns will experimentally correct for residual uncertainties in the implosion and hohlraum physics used in our radiation-hydrodynamic computational models using a variety of ignition capsule surrogates before proceeding to cryogenic-layered implosions and ignition experiments. The quantitative goals and technique options and down selections for the tuning campaigns are first explained. The computationally derived sensitivities to key laser and target parameters are compared to simple analytic models to gain further insight into the physics of the tuning techniques. The results of the validation of the tuning techniques at the OMEGA facility [J. M. Soures et al., Phys. Plasmas 3, 2108 (1996)] under scaled hohlraum and capsule conditions relevant to the ignition design are shown ...
Physics of Plasmas | 2014
O. A. Hurricane; D. A. Callahan; D. T. Casey; E. L. Dewald; T. R. Dittrich; T. Döppner; M. A. Barrios Garcia; D. E. Hinkel; L. Berzak Hopkins; P. Kervin; J. L. Kline; S. Le Pape; T. Ma; A. G. MacPhee; J. L. Milovich; J. D. Moody; A. Pak; P. K. Patel; H.-S. Park; B. A. Remington; H. F. Robey; J. D. Salmonson; P. T. Springer; R. Tommasini; L. R. Benedetti; J. A. Caggiano; Peter M. Celliers; C. Cerjan; Rebecca Dylla-Spears; D. H. Edgell
The “High-Foot” platform manipulates the laser pulse-shape coming from the National Ignition Facility laser to create an indirect drive 3-shock implosion that is significantly more robust against instability growth involving the ablator and also modestly reduces implosion convergence ratio. This strategy gives up on theoretical high-gain in an inertial confinement fusion implosion in order to obtain better control of the implosion and bring experimental performance in-line with calculated performance, yet keeps the absolute capsule performance relatively high. In this paper, we will cover the various experimental and theoretical motivations for the high-foot drive as well as cover the experimental results that have come out of the high-foot experimental campaign. At the time of this writing, the high-foot implosion has demonstrated record total deuterium-tritium yields (9.3×1015) with low levels of inferred mix, excellent agreement with implosion simulations, fuel energy gains exceeding unity, and evidenc...
Physics of Plasmas | 2012
Damien G. Hicks; N. B. Meezan; E. L. Dewald; A. J. Mackinnon; R.E. Olson; D. A. Callahan; T. Döppner; L. R. Benedetti; D. K. Bradley; Peter M. Celliers; D. S. Clark; P. Di Nicola; S. N. Dixit; E. G. Dzenitis; J. E. Eggert; D. R. Farley; J. A. Frenje; S. Glenn; S. H. Glenzer; Alex V. Hamza; R. F. Heeter; J. P. Holder; N. Izumi; D. H. Kalantar; S. F. Khan; J. L. Kline; J. J. Kroll; G. A. Kyrala; T. Ma; A. G. MacPhee
Measurements have been made of the in-flight dynamics of imploding capsules indirectly driven by laser energies of 1–1.7 MJ at the National Ignition Facility [Miller et al., Nucl. Fusion 44, 228 (2004)]. These experiments were part of the National Ignition Campaign [Landen et al., Phys. Plasmas 18, 051002 (2011)] to iteratively optimize the inputs required to achieve thermonuclear ignition in the laboratory. Using gated or streaked hard x-ray radiography, a suite of ablator performance parameters, including the time-resolved radius, velocity, mass, and thickness, have been determined throughout the acceleration history of surrogate gas-filled implosions. These measurements have been used to establish a dynamically consistent model of the ablative drive history and shell compressibility throughout the implosion trajectory. First results showed that the peak velocity of the original 1.3-MJ Ge-doped polymer (CH) point design using Au hohlraums reached only 75% of the required ignition velocity. Several capsu...
Physics of Plasmas | 2012
O. S. Jones; C. Cerjan; M. M. Marinak; J. L. Milovich; H. F. Robey; P. T. Springer; L. R. Benedetti; D. L. Bleuel; E. Bond; D. K. Bradley; D. A. Callahan; J. A. Caggiano; Peter M. Celliers; D. S. Clark; S. M. Dixit; T. Döppner; Rebecca Dylla-Spears; E. G. Dzentitis; D. R. Farley; S. Glenn; S. H. Glenzer; S. W. Haan; B. J. Haid; C. A. Haynam; Damien G. Hicks; B. J. Kozioziemski; K. N. LaFortune; O. L. Landen; E. R. Mapoles; A. J. Mackinnon
A detailed simulation-based model of the June 2011 National Ignition Campaign cryogenic DT experiments is presented. The model is based on integrated hohlraum-capsule simulations that utilize the best available models for the hohlraum wall, ablator, and DT equations of state and opacities. The calculated radiation drive was adjusted by changing the input laser power to match the experimentally measured shock speeds, shock merger times, peak implosion velocity, and bangtime. The crossbeam energy transfer model was tuned to match the measured time-dependent symmetry. Mid-mode mix was included by directly modeling the ablator and ice surface perturbations up to mode 60. Simulated experimental values were extracted from the simulation and compared against the experiment. Although by design the model is able to reproduce the 1D in-flight implosion parameters and low-mode asymmetries, it is not able to accurately predict the measured and inferred stagnation properties and levels of mix. In particular, the measu...
Review of Scientific Instruments | 2012
M. Gatu Johnson; J. A. Frenje; D. T. Casey; C. K. Li; F. H. Séguin; R. D. Petrasso; R. C. Ashabranner; R. Bionta; D. L. Bleuel; E. Bond; J. A. Caggiano; A. Carpenter; C. Cerjan; T. J. Clancy; T. Doeppner; M. J. Eckart; M. J. Edwards; S. Friedrich; S. H. Glenzer; S. W. Haan; Edward P. Hartouni; R. Hatarik; S. P. Hatchett; O. S. Jones; G. A. Kyrala; S. Le Pape; R. A. Lerche; O. L. Landen; T. Ma; A. J. Mackinnon
DT neutron yield (Y(n)), ion temperature (T(i)), and down-scatter ratio (dsr) determined from measured neutron spectra are essential metrics for diagnosing the performance of inertial confinement fusion (ICF) implosions at the National Ignition Facility (NIF). A suite of neutron-time-of-flight (nTOF) spectrometers and a magnetic recoil spectrometer (MRS) have been implemented in different locations around the NIF target chamber, providing good implosion coverage and the complementarity required for reliable measurements of Y(n), T(i), and dsr. From the measured dsr value, an areal density (ρR) is determined through the relationship ρR(tot) (g∕cm(2)) = (20.4 ± 0.6) × dsr(10-12 MeV). The proportionality constant is determined considering implosion geometry, neutron attenuation, and energy range used for the dsr measurement. To ensure high accuracy in the measurements, a series of commissioning experiments using exploding pushers have been used for in situ calibration of the as-built spectrometers, which are now performing to the required accuracy. Recent data obtained with the MRS and nTOFs indicate that the implosion performance of cryogenically layered DT implosions, characterized by the experimental ignition threshold factor (ITFx), which is a function of dsr (or fuel ρR) and Y(n), has improved almost two orders of magnitude since the first shot in September, 2010.
Physics of Plasmas | 2010
D. G. Hicks; B. K. Spears; D. G. Braun; R. E. Olson; C. Sorce; Peter M. Celliers; G. W. Collins; O. L. Landen
The velocity and remaining ablator mass of an imploding capsule are critical metrics for assessing the progress toward ignition of an inertially confined fusion experiment. These and other convergent ablator performance parameters have been measured using a single streaked x-ray radiograph. Traditional Abel inversion of such a radiograph is ill-posed since backlighter intensity profiles and x-ray attenuation by the ablated plasma are unknown. To address this we have developed a regularization technique which allows the ablator density profile ρ(r) and effective backlighter profile I0(y) at each time step to be uniquely determined subject to the constraints that ρ(r) is localized in radius space and I0(y) is delocalized in object space. Moments of ρ(r) then provide the time-resolved areal density, mass, and average radius (and thus velocity) of the remaining ablator material. These results are combined in the spherical rocket model to determine the ablation pressure and mass ablation rate during the implos...
Physics of Plasmas | 2014
A. L. Kritcher; R. P. J. Town; D. K. Bradley; D. S. Clark; B. K. Spears; O. S. Jones; S. W. Haan; P. T. Springer; J. D. Lindl; R. H. H. Scott; D. A. Callahan; M. J. Edwards; O. L. Landen
We investigate yield degradation due to applied low mode P2 and P4 asymmetries in layered inertial confinement fusion implosions. This study has been performed with a large database of >600 2D simulations. We show that low mode radiation induced drive asymmetries can result in significant deviation between the core hot spot shape and the fuel ρR shape at peak compression. In addition, we show that significant residual kinetic energy at peak compression can be induced by these low mode asymmetries. We have developed a metric, which is a function of the hot spot shape, fuel ρR shape, and residual kinetic energy at peak compression, that is well correlated to yield degradation due to low mode shape perturbations. It is shown that the ρR shape and residual kinetic energy cannot, in general, be recovered by inducing counter asymmetries to make the hot core emission symmetric. In addition, we show that the yield degradation due to low mode asymmetries is well correlated to measurements of time dependent shape throughout the entire implosion, including early time shock symmetry and inflight fuel symmetry.
Physics of Plasmas | 2010
R. Betti; P.-Y. Chang; B. K. Spears; Karen S. Anderson; John Edwards; M. Fatenejad; J. D. Lindl; R. L. McCrory; R. Nora; D. Shvarts
The physics of thermonuclear ignition in inertial confinement fusion (ICF) is presented in the familiar frame of a Lawson-type criterion. The product of the plasma pressure and confinement time Pτ for ICF is cast in terms of measurable parameters and its value is estimated for cryogenic implosions. An overall ignition parameter χ including pressure, confinement time, and temperature is derived to complement the product Pτ. A metric for performance assessment should include both χ and Pτ. The ignition parameter and the product Pτ are compared between inertial and magnetic-confinement fusion. It is found that cryogenic implosions on OMEGA [T. R. Boehly et al., Opt. Commun. 133, 495 (1997)] have achieved Pτ∼1.5 atm s comparable to large tokamaks such as the Joint European Torus [P. H. Rebut and B. E. Keen, Fusion Technol. 11, 13 (1987)] where Pτ∼1 atm s. Since OMEGA implosions are relatively cold (T∼2 keV), their overall ignition parameter χ∼0.02–0.03 is ∼5× lower than in JET (χ∼0.13), where the average temp...