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Hassan Naseh

Observed names: H Naseh, H. Naseh, hassan Naseh
ORCID: 0000-0002-7896-0189
Observed ORCID: 0000-0002-7896-0189
OpenAlex ID: A5033008025
A multi-objective, multidisciplinary design optimization methodology for the conceptual design of a spacecraft bi-propellant propulsion system
2015 · H. R. Fazeley, H. Taei, et al. · Structural and Multidisciplinary Optimization · 20
A novel framework for liquid propellant engine’s cooling system design by sensitivity analysis based on RSM and multi-objective optimization using PSO
2020 · H.R. Alimohammadi, H. Naseh, et al. · Advances in Space Research · 15
Progressive Latin Hypercube sampling-based robust design optimisation (PLHS-RDO)
2020 · M. N. P. Meibody, H. Naseh, et al. · Australian Journal of Mechanical Engineering · 15
An integrated methodology applied for reliability based multi-disciplinary design optimization in EPFE with LOX/kerosene
2023 · H.R. Alimohammadi, H. Naseh, et al. · Reliability Engineering & System Safety · 14
Liquid propellant engine conceptual design by using a fuzzy-multi-objective genetic algorithm (MOGA) optimization method
2014 · M Mirshams, H Naseh, et al. · Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering · 10
A new synthetic metamodel methodology for liquid‐propellant engine's cooling system optimization
2020 · Hamid Reza Alimohammadi, Hassan Naseh, et al. · Heat Transfer · 9
A kriging based multi objective gray wolf optimization for hydrazine catalyst bed
2019 · M. N. P. Meibody, H. Naseh, et al. · Engineering Solid Mechanics · 9
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Developing a Multi-objective Multi-Disciplinary Robust Design Optimization Framework
2021 · M. N. P. Meibody, H. Naseh, et al. · Scientia Iranica · 8
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A Bayesian networks approach to reliability analysis of a space vehicle separation sub-system
2013 · H. Naseh, M. Mirshams · International Conference on Recent Advances in Space Technologies · 8
Design of Physical Configuration of a 10N Monopropellant Hydrazine Thruster
2019 · Hadiseh Karimaei, Mohammad Reza Salimi, et al. · علوم و فناوری فضایی · 5
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An Analytic Hierarchy Process Based Reliability Allocation Method (aram)
2011 · A. M. Akhlaghi, H. Naseh, et al. · ISAHP proceedings · 4
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Space Mission Definition Based on Analytical Hierarchy Process (ahp) Method
2018 · Hassan Naseh · International Journal of the Analytic Hierarchy Process · 3
A Bayesian Networks Approach to Reliability Analysis of a Launch Vehicle Liquid Propellant Engine
2011 · A. M. Akhlaghi, Hassan Naseh, et al. · Jour of Aerospace Science and Technology · 3
Sensitivity analysis based on Progressive LHS Applied to Hydrazine Catalyst Bed Design
2019 · Mohammad Naddafi Pour Meibody, Hassan Naseh, et al. · علوم و فناوری فضایی · 2
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Catalyst bed multi-objective optimization
2019 · H Naseh, MNP Meibody, et al. · Aeronautics and Aerospace Open Access Journal · 2
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Numerical-parametrical analysis on the hydrogen peroxide catalyst bed for space monopropellant thruster applications
2018 · Hassan Naseh, mohamamd M.N.P. Meibody, et al. · 2
Integrated high-fidelity model - machine learning framework to reliability-based metamodel development
2025 · M.H. Mansuri Mughari, H. Naseh, et al. · Reliability Engineering & System Safety · 1
An adaptive hybrid kriging–RSM approach to enhance the surrogate-based MDO accuracy for re-entry bio-capsules
2025 · Hassan Naseh, Hadiseh Karimaei, et al. · Advances in Space Research · 1
Applying ergonomics for beyond the earth: Integrating participatory ergonomic design for sending a human to space
2023 · Hossein Beiranvand, Mahmood Ayoobi, et al. · Work · 1
Adaptive surrogate modelling algorithm for meta-model-based design optimisation
2021 · M.N.P. Meibody, H. Naseh, et al. · International Journal of Industrial and Systems Engineering · 1
Propellant Management Device (PMD) Design Optimization of Hydrazine Fuel Tank
2017 · Hassan Naseh, Ali Alipour · مهندسی مکانیک مدرس · 1
Reliability Allocation to Launch Vehicle Subsystems by Using Ahp Method in Conceptual Design Phase
2012 · Mehran Mirshams, Shahrukh A. Irani, et al. · DOAJ (DOAJ: Directory of Open Access Journals) · 1
A surrogate model development for design optimization of thrust chamber
2026 · H. R. Alimohammadi, H. Naseh, et al. · Aerospace Systems
An efficient variance-based approach in RMDO framework of a space capsule under material and manufacturing uncertainties
2025 · Hassan Naseh, Hadiseh Karimaei, et al. · Reliability Engineering & System Safety
Novel synthesis optimisation framework based on performance prediction model for a space propulsion system
2025 · M. H. Mansuri Mughari, H. Naseh, et al. · The Aeronautical Journal
Works count: 44
Citation count: 139
H-index: 8
I10-index: 5
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