Hassan Naseh

Sample image

 

Assistant Professor

Ph.D.  Department of Aerospace Engineering, K. N. Toosi University of Technology, Tehran, Iran

Dissertation: Space Launch System Conceptual Design by using Holistic Concurrent Design

 

M.Sc. 

Thesis: 

 

B.Sc. 

Senior project: 

 

Google scholar address

Tel:  

Email: This email address is being protected from spambots. You need JavaScript enabled to view it.  , This email address is being protected from spambots. You need JavaScript enabled to view it.

Web Site Address: http://ari.ac.ir/hnaseh

 


Research Interests 

 • Space System Design and Engineering.

• Orbital Mechanics

• Satellites and Applications

• Space Launch System Conceptual Design 

• Multidisciplinary Design Optimization (MDO)

• Reliability based Design

 

 

Publications

 Journal Papers:

1. Mahyari M. N., Karimi H., Naseh H., Mirshams M., “Numerical and Experimental Investigation of Vortex Breaker Effectiveness on the Improvement in Launch Vehicle Ballistic Parameters,” Journal of Mechanical Science and Technology, KSME & Springer, 2010.

2. M. Mirshams, H. Naseh, H. R. Fazeli, “Multi-objective Multidisciplinary design of Space Launch System using Holistic Concurrent Design”, Journal of Aerospace, Science and Technology, 2014.

3. M. Mirshams, H. Naseh, H. Taei, H. R. Fazeli, “Liquid Propellant Engine Design by Using a Fuzzy - Genetic Algorithm Multi-objective Optimization Method”, Journal of Imech. Part G, Journal of Aerospace Engineering, 2014.

4. H. R. Fazeli, H. Taei, H. Naseh, M. Mirshams A multi-objective, multidisciplinary design optimization methodology for the conceptual design of a spacecraft bi-propellant propulsion system,  Springer, 2015

5. Afshari H. H., Naseh H., Novinzade A. R. and Roushanian J., “A Variational Approach in Determination of Explicit Neighboring Optimal Guidance Law for Injection into Orbit,” International Journal of Review of Automatic Control, 2008.

6. Akhlaghi A. M., Naseh H., Mirshams M., Irani S., A Bayesian Networks Approach to Reliability Analysis of a Launch Vehicle Liquid Propellant Engine, Journal of Aerospace and Technology (JAST), 2012.

7. Mirshams M.,  Karimi H. and Naseh H., “Multi-stage Liquid Propellant Launch Vehicle Conceptual Design,” Journal of Space Science and Technology (JSST), Vol. 1, No. 1, 2008 (Persian).

8. Mirshams M.,  Karimi H. and Naseh H.,“Launch Vehicle Conceptual Design (LVCD) Software,” Journal of Space Science and Technology (JSST), Vol. 2, No. 1, 2008 (Persian).

9. M. Mirshams, S. Irani, A. M. Akhlaghi, H. Naseh, “Reliability Allocation to Launch Vehicle Subsystems by Using AHP Method in conceptual design phase", Journal of Space Science and Technology (JSST), Vol. 2, No. 1, 2012 (Persian).

10. M. Mirshams, H. Naseh, A. M. Akhlaghi, S. Irani, “Space launch System Reliability based design Methodology", Journal of Science and Research Sharif, 2013 (Persian).

11. M. Mirshams, H. Naseh, H. R. Fazeli, Multi-objective Multidisciplinary design of Space Launch System using Holistic Concurrent Design, Journal of Aerospace, Science and Technology, Dec. 2013 (ISI Journal).

12. H. R. Fazeli, H. Taei, H. Naseh, M. Mirshams A multi-objective, multidisciplinary design optimization methodology for the conceptual design of a spacecraft bi-propellant propulsion system, Journal of structural and Multidisciplinary Optimization, 2015 (ISI Journal).

13. M. Mirshams, H. Naseh, H. Taei, H. R. Fazeli, Liquid Propellant Engine Design by Using a Fuzzy - Genetic Algorithm Multi-objective Optimization Method, Journal of Aerospace Engineering, Jan. 2014 (ISI Journal).

 

 Books:

 Book Chapters:

 Conference Papers:

1. M. N. Mahyari, H. Karimi, Naseh H., M. Mirshams " Study of Using Vortex Breakdown in Vortical Flow Field at the Outlet of Propellant Tanks", Accepted in the Ninth International Congress of Fluid Dynamics & Propulsion December 18 2008

2. Naseh H., A. Akhlaghi, M. Mirshams, S. Irani, A Bayesian Networks Approach to Reliability Analysis of a Launch Vehicle GN&C, 14-16 September 2011 - METU, Ankara TURKEY.

3. Naseh H., A. M. Akhlaghi, M. Mirshams, S. Irani, An Analytic Hierarchy Process based Reliability Allocation Method (ARAM), International Symposium on the Analytic Hierarchy Process 2011, Italy, Sorento.

4. Naseh H., M. Mirshams, “A Bayesian Networks Approach to Reliability Analysis of a Launch Vehicle Separation Subsystem”, 12-14 June 2013 -RAST, Istanbul TURKEY.

 

 

Teaching Experiences

 

• Advanced Numerical Methods, Dep. Of Aerospace Eng. K. N. Toosi Univ. Of Tech.(Fall)

• Differential Equations, Dep. Of Aerospace Eng. K. N. Toosi Univ. Of Tech.(Fall)    

• Advanced Space Transportation System Design, Dep. Of Aerospace Eng. K. N. Toosi Univ. Of Tech.(winter)

• Airplane Mechanic of Flight, Dep. Of Aerospace. Eng. K. N. Toosi Univ. Of Tech.(winter)

 

Research Supervision

 

 

 

 

Professional Experiences

 

1. Best Student Researcher Award, K. N. Toosi University of Technology, Mechanical and Aerospace Engineering Faculty (Research Ceremony, 2006).

2. Finalist for Best Paper Award at the 7th International Conference Society of Aerospace (2007).

 

 

 
 
You are here: ARI About ARI People Faculty Hassan Naseh