Thermal performance of foam/MLI for cryogenic liquid hydrogen tank during the ascent and on orbit period
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Systems designed for measuring effective thermal conductivity of MLI mostly use the rate of evaporation of a cryogen.
“Systems designed for measuring effective thermal conductivity of MLI are mostly using the rate of evaporation of a cryogen [4,5,6,7].”
From Design of a multi-layer insulation(MLI) measurement system with a G-M cryocooler (2019) · cites this paper as [5]
Spray-on foam insulation and hollow-glass microsphere show no significant difference in thermal conductivity under vacuum or non-vacuum conditions, so they can play a crucial role when vacuum insulation faults occur.
“Both spray-on foam insulation and hollow-glass microsphere show no significant difference in thermal conductivity under vacuum or non-vacuum conditions; therefore, they can play a crucial role considering faults in vacuum insulation [116]”
From 5917. https://doi.org/10.3390/en14185917. - (2021) · cites this paper as [116]
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(2021) · doi:10.3390/en14185917 · Cited by 708 · see citing works
Design of a multi-layer insulation(MLI) measurement system with a G-M cryocooler
Li, X., Xu, D., Shen, F., Liu, H., & Li, L. (2019) · IOP Conference Series: Materials Science and Engineering · doi:10.1088/1757-899x/502/1/012075 · Cited by 7 · see citing works
- Authors
- Liu, Z., Li, Y., Xie, F., & Zhou, K.
- Affiliations
- Xi'an Jiaotong University (CN)
- State Key Laboratory of Technologies in Space Cryogenic Propellants (CN)
- Corresponding author
- Li, Yanzhong
- Venue
- Applied Thermal Engineering
- Publisher
- Elsevier BV
- Published
- 2016-04
- Volume
- 98
- Pages
- 430-439
- ISSN
- 1359-4311 (ISSN-L)
- OpenAlex
- W2203880498
- Cited by
- 59
- References
- 0
- Citations by year
- 2026: 7 · 2025: 8 · 2024: 12 · 2023: 9 · 2022: 3 · 2021: 4 · 2020: 2 · 2019: 8 · 2018: 3 · 2017: 1 · 2016: 2
- FWCI
- 2.90
- Type
- journal article
- Language
- en
- Open access
- closed
- Locations
- Applied Thermal Engineering (publishedVersion)
- Funders
- National Natural Science Foundation of China (51376142)
- Research Fund of State Key Laboratory of Technologies in Space Cryogenic Propellants (SKLTSCP1505)
- Topics
- Physical Sciences › Engineering › Aerospace Engineering › Spacecraft and Cryogenic Technologies
- Physical Sciences › Engineering › Aerospace Engineering › Spacecraft Design and Technology
- Physical Sciences › Mathematics › Applied Mathematics › Gas Dynamics and Kinetic Theory
- Keywords
- multilayer insulation, thermal insulation, heat leakage, thermal resistance, quasi-steady-state model, heat transfer modes
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Registry, retraction, Cites and statistics results are computed, not judged, with one exception: a printed reference that no index lists is read once by a model before it counts as a citation error. Claims are extracted by a model and kept only when their quote appears verbatim in the text; each cited source is then checked, with a model’s help, for whether it says what the claim relies on. Those verdicts can be wrong — read the claim’s quote and the cited source before relying on one.
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