Cited by 96Spacecraft and Cryogenic TechnologiesAerogels and thermal insulationThermal properties of materials

The DOI matches its Crossref record.

Modeling and experimental study on combination of foam and variable density multilayer insulation for cryogen storage

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Crossref · 10.1016/j.energy.2017.01.147

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Citations

Cites

No references could be resolved yet.

Research works printed but not linked: 13

  1. Hedayat, 2002, Analytical modeling of variable density multilayer insulation for cryogenic storage, Adv Cryog Eng, 47, 1557, 10.1063/1.1472190 · DOI
  2. Barrios, 2013, Thermal conductivity of rigid foam insulations for aerospace vehicles, Cryogenics, 55, 12, 10.1016/j.cryogenics.2012.11.004 · DOI · Paper page
  3. Barrios, 2012, Thermal conductivity of spray-on foam insulations for aerospace applications, Adv Cryog Eng, 1434, 1319
  4. Fesmire, 2012, Spray-on foam insulations for launch vehicle cryogenic tanks, Cryogenics, 52, 251, 10.1016/j.cryogenics.2012.01.018 · DOI · Paper page
  5. Fesmire, 2008, Aerogel insulation applications for liquid hydrogen launch vehicle tanks, Cryogenics, 48, 223, 10.1016/j.cryogenics.2008.03.014 · DOI · Paper page
  6. Zhang, 2012, Experimental study on cryogenic moisture uptake in polyurethane foam insulation material, Cryogenics, 52, 810, 10.1016/j.cryogenics.2012.10.001 · DOI
  7. Li, 2006, Thermal analysis and performance study for multilayer perforated insulation material used in space, Appl Therm Eng, 26, 2020, 10.1016/j.applthermaleng.2006.01.004 · DOI
  8. Hastings, 1998, Experimental testing of a foam/multilayer insulation (FMLI) thermal control system (TCS) for use on a cryogenic upper stage, Space Technol Appl Int Forum, 420, 331
  9. Johnson, 2010, Analysis and testing of multilayer and aerogel insulation configurations, Adv Cryog Eng, 1218, 780
  10. Liu, 2016, Thermal performance of foam/MLI for cryogenic liquid hydrogen tank during the ascent and on orbit period, Appl Therm Eng, 98, 430, 10.1016/j.applthermaleng.2015.12.084 · DOI · Paper page
  11. McIntosh, 1994, Layer by layer MLI calculation using a separated mode equation, Adv Cryog Eng, 39, 1683, 10.1007/978-1-4615-2522-6_206 · DOI · Paper page
  12. Tseng, 1997, Thermal conductivity of polyurethane foams from room temperature to 20 K, Cryogenics, 37, 305, 10.1016/S0011-2275(97)00023-4 · DOI · Paper page
  13. Wang, 2016, Optimization of variable density multilayer insulation for cryogenic application and experimental validation, Cryogenics, 80, 154, 10.1016/j.cryogenics.2016.10.006 · DOI

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Metadata

Authors
Huang, Y., Wang, B., Zhou, S., Wu, J., Lei, G., Li, P., & Sun, P.
Affiliations
  • Shanghai Jiao Tong University (CN)
  • State Key Laboratory of Technologies in Space Cryogenic Propellants (CN)
Corresponding author
Huang, Yonghua
Venue
Energy
Publisher
Elsevier BV
Published
2017-03
Volume
123
Pages
487-498
ISSN
0360-5442 (ISSN-L)
OpenAlex
W2585543744
Cited by
96
References
0
Citations by year
2026: 18 · 2025: 19 · 2024: 13 · 2023: 15 · 2022: 7 · 2021: 7 · 2020: 6 · 2019: 8 · 2018: 3
FWCI
4.28
Type
journal article
Language
en
Open access
closed
Locations
  • Energy (publishedVersion)
  • RePEc: Research Papers in Economics (submittedVersion)
Funders
  • National Natural Science Foundation of China (51676118)
  • State Key Laboratory of Technologies (SKLTSCP1206-W/20130118)
Topics
  • Physical Sciences › Engineering › Aerospace Engineering › Spacecraft and Cryogenic Technologies
  • Physical Sciences › Materials Science › Materials Chemistry › Aerogels and thermal insulation
  • Physical Sciences › Materials Science › Materials Chemistry › Thermal properties of materials
Keywords
cryogenic propellant storage, multilayer insulation, polyurethane foam, thermal performance modeling, apparent thermal conductivity, heat flux, aerogels

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