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Stream/Area:
-
Subject:
-
Paper ID:
IJSREM67638
Volume:
10 |
10 |
Oct 2026
Pages:
1-52
Publication Frequency:
Monthly (12 issues per year)
License:International Journal of Scientific Research in Engineering and Management follows the Creative Commons Attribution 4.0 (CC BY 4.0) License, allowing free use and distribution with proper attribution.
M.E Cryogenic Engineering
PSN college of Engineering and Technology (Autonomous)
M.E Cryogenic Engineering
PSN college of Engineering and Technology (Autonomous)
M.E Cryogenic Engineering
PSN college of Engineering and Technology (Autonomous)
M.E Cryogenic Engineering
PSN college of Engineering and Technology (Autonomous)
M.E Cryogenic Engineering
PSN college of Engineering and Technology (Autonomous)
Liquid hydrogen (LH₂) is a promising clean energy carrier because of its high energy density and zero carbon emissions during utilization. However, due to its extremely low boiling temperature (20 K), significant heat leakage into storage tanks causes hydrogen boil-off, reducing storage efficiency and increasing operational losses. Multi-Layer Insulation (MLI) is one of the most effective thermal insulation techniques for minimizing heat transfer in cryogenic storage systems. This project aims to numerically investigate the thermal performance of MLI systems applied to liquid hydrogen storage tanks using finite element analysis. The study focuses on modelling conductive and radiative heat transfer through different MLI configurations. Various parameters including the number of insulation layers, layer spacing, vacuum pressure, and material properties will be analysed to determine their influence on heat leakage and temperature distribution. Numerical simulations will be performed using ANSYS Steady-State Thermal to estimate the overall heat flux and optimize insulation performance. The expected outcome is an optimized MLI design capable of minimizing heat ingress while maintaining structural feasibility. The numerical results will be validated with published literature to ensure reliability. The findings are expected to contribute toward the development of highly efficient cryogenic storage systems for hydrogen-powered transportation and aerospace applications.
KEYWORDS
The present project, titled “Numerical Simulation and Thermal Optimization of Multi-Layer Insulation (MLI) Systems for Cryogenic Liquid Hydrogen Storage Tanks,” focused on studying the thermal behaviour of MLI used to minimize heat transfer into cryogenic liquid hydrogen storage systems. Since liquid hydrogen must be maintained at an extremely low temperature, effective thermal insulation is essential to reduce heat leakage and minimize evaporation or boil-off losses. The study considered the important MLI parameters such as number of insulation layers, layer density, surface emissivity, insulation thickness and vacuum conditions. The numerical simulation approach provides an effective method for predicting the temperature distribution, heat flux and heat leakage through the insulation system. By varying the important design parameters, the influence of each parameter on the thermal performance of the storage tank can be evaluated. The analysis shows that increasing the number of reflective layers can reduce radiation heat transfer; however, excessive layer density may increase solid conduction. Therefore, an optimum number of layers and suitable layer spacing are required to achieve improved insulation performance. The study also highlights the importance of maintaining a sufficiently high vacuum around the MLI system. A good vacuum reduces gas conduction between the insulation layers and improves the overall thermal resistance. Similarly, the use of low-emissivity reflective materials helps reduce radiation heat transfer. Proper control of layer density, vacuum pressure and material properties is therefore essential for achieving minimum heat leak and lower liquid hydrogen boil-off. The optimized MLI system can provide several benefits, including reduced heat leakage, lower hydrogen boil-off rate, improved storage efficiency, reduced refrigeration requirements and better thermal stability. The use of numerical simulation also reduces the need for repeated physical prototypes because different insulation configurations can be evaluated before fabrication. This makes the design and optimization process more economical and time-efficient. Overall, MLI is a highly effective insulation technique for cryogenic liquid hydrogen storage applications when it is properly designed, installed and maintained under suitable vacuum conditions. The numerical and optimization approach presented in this project provides a useful foundation for developing efficient cryogenic storage systems. Further experimental validation, advanced material selection, coupled thermal-structural analysis and AI-based optimization can improve the accuracy and practical applicability of the proposed system in future work.
1. Johnson, W. L., “Thermal Performance of Cryogenic Multilayer Insulation at Various Layer Spacings,” NASA Technical Reports Server, NASA Glenn Research Center. 2. Johnson, W. L., “Review of MLI Behavior at Low Temperatures and Application to L'Ralph Thermal Modeling,” NASA Technical Reports Server, 2019. 3. Mital, S. K., Gyekenyesi, J. Z., Arnold, S. M., Sullivan, R. M., Manderscheid, J. M. and Murthy, P. L. N., “Review of Current State of the Art and Key Design Issues With Potential Solutions for Liquid Hydrogen Cryogenic Storage Tank Structures for Aircraft Applications,” NASA/TM-2006-214346, NASA Glenn Research Center, 2006. 4. Johnson, W. L., “Robust Multilayer Insulation for Cryogenic Systems,” NASA Technical Reports Server, NASA Kennedy Space Center. 5. Marlow, W. A., “Design of Multilayer Insulation for the Multipurpose Hydrogen Test Bed,” NASA Marshall Space Flight Center, 2011. 6. “Integrated Multilayer Insulation,” NASA Technical Reports Server, NASA Kennedy Space Center. 7. “A Review of Candidate Multilayer Insulation Systems for Potential Use on Wet-Launched LH₂ Tankage for the Space Exploration Initiative Lunar Missions,” NASA Technical Reports Server. 8. “Multilayer Insulation Thermal Protection Systems Technology,” NASA Marshall Space Flight Center, NASA Technical Report, 1971. 9. “Improved Thermal-Insulation Systems for Low Temperatures,” NASA Technical Reports Server. 10. “Testing Seam Concepts for Advanced Multilayer Insulation,” NASA Glenn Research Center, NASA Technical Reports Server.
Publication Date
10/3/2026
Peer Review Type
Double-Blind Peer Review
Review Rounds: 2
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