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Visit Chief Executive Officer of Iranian Space Research Center from Space Research Lab.

2019-01-02T07:05:27+00:00

Visit Chief Executive Officer of Iranian Space Research Center from Space Research Lab. On December 9th, 2018 On December 9, 2018, the Chair of the Iranian Space Research Center, Dr. Samimi, along with the accompanying delegation (Mr. Dr. Jafar Salihi, Dr. Abdollahi, Dr. Libibian, Dr. Reisi) and with the presence of the chairman of the Faculty of Aerospace Engineering, Mr. Karimi Mazareeshahi, at a three Hours visit from the Space Research Laboratory, visited the capabilities and achievements of the complex and were briefed in the progress of the SSS-1 project.In this event, Dr. Mehran Mirshams, head of the Space Research Laboratory, [...]

Visit Chief Executive Officer of Iranian Space Research Center from Space Research Lab. 2019-01-02T07:05:27+00:00

A Thesis Defense Session for MSc/Zahra Hoodan

2018-10-31T10:58:57+00:00

Title: CubeSat Lunar Mission Design By Zahra Hoodan Supervisor: Dr. Mehran Mirshams Chairmen: Dr. Hasan Naseh (Aerospace Research Institute), Dr. Mahdi Jafari Nadoushan (K. N. Toosi University of Technology) September 12, 2018 Space exploration and travelling to The Moon and Mars, was the topic of world space week in 2017, and also the 2019-year theme will be "The Moon: Gateway to the stars". Furthermore, the space society's approach to using cubesats and the KNTU student cubesat team Nasir-1's participating in student Iranian cube competition from ISA, were the starting point to formation of this thesis idea "Lunar [...]

A Thesis Defense Session for MSc/Zahra Hoodan 2018-10-31T10:58:57+00:00

A Thesis Defense Session for MSc/Sara Mirshekari

2018-09-22T12:09:18+00:00

Title: GEO communication satellites reliability analysis based on operational life By Sara MirshekariSupervisor: Dr. Mehran MirshamsAdvisor: Dr. Ehsan ZabihianChairman: Dr. Saeid Irani (K. N. Toosi University of Technology), Dr. Hasan Naseh (Aerospace Research Institute)September 11, 2018 Abstract: The geosynchronous satellites as a complicated system with high lifetime in order to design and manufacturing need to certain and step by step process allocation and analysis of reliability. Regard to type and importance of mission complexity, operational longevity and also impossibility for repairing and maintaining at time of operation, it is very important to consider all aspects (dimensions) of failure [...]

A Thesis Defense Session for MSc/Sara Mirshekari 2018-09-22T12:09:18+00:00

A Thesis Defense Session for MSc/Negin Abbas Rezaei

2018-09-23T06:25:09+00:00

Title: Conceptual design of GEO communication all electric satellite By Negin Abbas RezaeiSupervisor: Dr. Mehran MirshamsAdvisor: Soheil S. ZamaniChairmen: Dr. Ali Jafarsalehi, Dr. Mahdi Jafari Nadoushan (K. N. Toosi University of Technology)September 11, 2018 The purpose of this thesis is the conceptual design of all-electric telecommunication satellites in GEO orbits. The design method uses statistical and parametric modeling. Statistical models are based on data analysis of all telecommunication satellites, as well as hybrid and chemical, from 2015 to June 2018. Parametric models have been used to increase the accuracy of the underlying design with the combination of existing classical models. [...]

A Thesis Defense Session for MSc/Negin Abbas Rezaei 2018-09-23T06:25:09+00:00

A Thesis Defense Session for MSc/Mahdi Bayat

2018-09-23T06:42:53+00:00

Title: Systematic Design of a Satellite with Design Structure Matrix (DSM) Method By Mahdi BayatSupervisor: Dr. Mehran MirshamsAdvisor: E. Sajad GhazanfarniaChairman: September 11, 2018 Abstract The purpose of this study is to introduce and propose design structure matrix in the conceptual designing phase for CubeSats. The designing process began from eliciting performance parameters and culminated in the formation of design structure matrix, determining dependencies and finally their optimization. Optimization of design structure matrix includes achieving designing sequence, control of interferences and designing parameters determined for the satellite. This method has been applied on a CubeSat with three units. Designing a three-unit [...]

A Thesis Defense Session for MSc/Mahdi Bayat 2018-09-23T06:42:53+00:00

Contact Info

Space Research Laboratory, Aerospace Engineering Faculty, K. N. Toosi University of Technology, Daneshgah Blvd., Ehsan Exit, East Zeynoddin Highway, Tehran, Iran

Phone: +98 21 77334133

Fax: +98 21 73064234

Web: Spacerl

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