Cited by 73Gas Dynamics and Kinetic TheorySpacecraft Design and TechnologyHeat Transfer and Mathematical Modeling

Thermal Analysis and Design Optimization of Multilayer Insulation for Reentry Aerodynamic Heating

Daryabeigi, Kamran·2002·Journal of Spacecraft and Rockets

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Crossref · 10.2514/2.3863

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  • Multi-layer insulation is considered the most effective way of heat insulation in high vacuum cryogenic systems and is widely utilized in these systems.

    “Multi-layer insulation is considered as the most effective way of heat insulation in high vacuum cryogenic systems and is widely utilized in these systems [1,2,3].”

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Authors
Daryabeigi, K.
Affiliations
Langley Research Center (US)
Corresponding author
Daryabeigi, Kamran
Venue
Journal of Spacecraft and Rockets
Published
2002-07
Volume
39
Issue
4
Pages
509-514
ISSN
  • 0022-4650 (ISSN-L)
  • 1533-6794
OpenAlex
W2019797834
Cited by
73
References
0
Citations by year
2026: 3 · 2025: 2 · 2024: 9 · 2023: 4 · 2022: 5 · 2021: 3 · 2019: 6 · 2018: 4 · 2017: 4 · 2016: 4 · 2015: 6 · 2014: 1 · 2013: 2 · 2012: 1
FWCI
3.48
Type
journal article
Language
en
Open access
closed
Locations
Journal of Spacecraft and Rockets (publishedVersion)
Topics
  • Physical Sciences › Mathematics › Applied Mathematics › Gas Dynamics and Kinetic Theory
  • Physical Sciences › Engineering › Aerospace Engineering › Spacecraft Design and Technology
  • Physical Sciences › Engineering › Mechanical Engineering › Heat Transfer and Mathematical Modeling
Keywords
multilayer insulation, thermal analysis, design optimization, spacecraft thermal protection, heat shields

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