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Proceedings ArticleDOI

Radiative Transfer in a Low Density Ablative Material under Arcjet Flow Conditions

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The article was published on 2017-01-09. It has received 1 citations till now. The article focuses on the topics: Arcjet rocket & Radiative transfer.

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Thermal Response Analysis of Porous Carbon-based Non-Ablative Heatshield in an Arcjet Flow Condition

TL;DR: In this article, a thermal response analysis of a non-ablative heat shield called the Non-Ablative Lightweight Thermal protection system (NALT), which is heated in an arcjet flow, is presented.
References
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Proceedings ArticleDOI

Phenolic Impregnated Carbon Ablators (PICA) for Discovery class missions

TL;DR: In this article, the authors present the development of the light weight Phenolic Impregnated Carbon Ablators (PICA) and its thermal performance in a simulated heating environment for planetary entry probes.
Journal ArticleDOI

Tomography-based Monte Carlo determination of radiative properties of reticulate porous ceramics

TL;DR: In this article, a 3D digital representation of a reticulate porous ceramic (RPC) sample, generated by computer tomography (CT), is employed to determine its porosity, surface-to-volume ratio, and the minimum size of a representative elementary volume (REV) for the continuum domain.
Journal ArticleDOI

Application of Integral Methods to Ablation Charring Erosion, A Review

TL;DR: In this paper, an application of approximate heat balance integral (HBI) methods to more realistic models of material response, specifically, for carbon-carbon and carbon-phenolic heat shields on reentry vehicles, is presented.
Journal ArticleDOI

Numerical study of iso-Q sample geometric effects on charring ablative materials

TL;DR: In this paper, the geometric effects of iso-Q sample geometry on charring ablative materials under arc-jet conditions were numerically studied, and the results indicated that the sample diameter, thickness, and sample holder affect the pyrolysis gas transport, thermal, and material response within the material.
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