Decoupled rocket model of a spherical shell implosion in inertial confinement fusion Article Swipe
YOU?
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· 2023
· Open Access
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· DOI: https://doi.org/10.1063/5.0173503
In inertial confinement fusion, the rocket model has achieved great success in describing many important effects, including the residual mass of the shell, average implosion velocity, the motion of the ablative surface, and rocket efficiency (the ratio of the kinetic energy of the shell to absorbed energy). This model uses only the implosion parameter to describe the spherical ablative implosion dynamics under the thin-shell assumption. In this paper, we introduce a decoupled rocket model using an additional parameter that extends beyond the thin-shell assumption to describe the implosion dynamics at the same time. This provides information for the theoretical design of a thick shell by optimizing two parameters rather than only one implosion parameter. To demonstrate this, we apply these two models to design single-shell targets driven by the same radiation source. Our simulations show the decoupled rocket model can get better theoretical design results in a larger parameter space.
Related Topics
- Type
- article
- Language
- en
- Landing Page
- https://doi.org/10.1063/5.0173503
- OA Status
- gold
- References
- 24
- Related Works
- 10
- OpenAlex ID
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Raw OpenAlex JSON
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https://openalex.org/W4387747101Canonical identifier for this work in OpenAlex
- DOI
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https://doi.org/10.1063/5.0173503Digital Object Identifier
- Title
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Decoupled rocket model of a spherical shell implosion in inertial confinement fusionWork title
- Type
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articleOpenAlex work type
- Language
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enPrimary language
- Publication year
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2023Year of publication
- Publication date
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2023-10-01Full publication date if available
- Authors
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Lulu Li, Ruihua Xu, Yingkui Zhao, Wu WenList of authors in order
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https://doi.org/10.1063/5.0173503Publisher landing page
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YesWhether a free full text is available
- OA status
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goldOpen access status per OpenAlex
- OA URL
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https://doi.org/10.1063/5.0173503Direct OA link when available
- Concepts
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Implosion, Rocket (weapon), Inertial confinement fusion, Physics, Spherical shell, Shell (structure), Mechanics, Parameter space, Aerospace engineering, Plasma, Computational physics, Classical mechanics, Nuclear physics, Mechanical engineering, Geometry, Engineering, MathematicsTop concepts (fields/topics) attached by OpenAlex
- Cited by
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0Total citation count in OpenAlex
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24Number of works referenced by this work
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10Other works algorithmically related by OpenAlex
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| referenced_works | https://openalex.org/W2080014950, https://openalex.org/W4311558945, https://openalex.org/W2064347425, https://openalex.org/W2077745612, https://openalex.org/W2313958482, https://openalex.org/W2002103877, https://openalex.org/W2091567034, https://openalex.org/W2080917063, https://openalex.org/W2163915153, https://openalex.org/W2083105683, https://openalex.org/W2036591517, https://openalex.org/W2016564921, https://openalex.org/W2000287528, https://openalex.org/W2066437041, https://openalex.org/W2914661502, https://openalex.org/W3197782525, https://openalex.org/W2950007056, https://openalex.org/W4213211395, https://openalex.org/W2176041599, https://openalex.org/W2575910356, https://openalex.org/W3135347816, https://openalex.org/W4226499614, https://openalex.org/W2967279378, https://openalex.org/W3183346302 |
| referenced_works_count | 24 |
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| sustainable_development_goals[0].display_name | Affordable and clean energy |
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