M. Sc. Thesis Author Introduction: First name: Zahra Last name: Hoodan Entrance year: 2015 Defense date: 2018/Sep/12 Email address: firstname.lastname@example.org Title: Cubesat Lunar Mission Design Abstract: In this thesis, the idea of having a mission to Moon using a cubesat and the process of mission design according to the defined steps, is presented. This process starts with presenting the mission definition and describing the parts that forms a mission. The mission analysis consists of describing the lunar mission objectives and constraints and also the idea of using Iranian Launch Vehicle, considering the mass constraint of third [...]
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Long Term -Mechanics of Materials -Orbital mechanics -Computer Aided Design -Aerospace System Design -Launch Vehicle System Design -Satellite System Design -Finite Elements Methods -Space Environments Short Term--Developing Next Generation Space Talent Short Term--Workshops
Project OverviewThe Nasir-1 CubeSat is designed and developed by Space Research Lab (SRL) of K.N. Toosi University of Technology (KNTU) within a Student CubeSat contest which is organized by the Iranian Space Agency (ISA). Currently, this project lies in the phase of the Engineering Model (Phase C, as per the ECSS standards).Nasir-1 CubeSat team is composed of university staff, M.Sc. and B.Sc. students from faculties of Aerospace, Electrical, and Computer Engineering under supervision of SRL technical team.The Nasir-1 CubeSat project is initially defined based on the technical requirements of the ISA and on the missions of ADS-B and ISL (with Gamalink [...]
Paper Presentation by: Ms. Sara Mirshekari Authors: Sara Mirshekari, Ehsan Zabihian, Mehran Mirshams, Peyman Nikpey Paper Title: Statistical GEO satellite's reliability analysis based on operational life time. Date: 31 December; 2018 Place: Tehran/Iranian Space Research Center (ISRC) Symposium: 4th Specialized Meeting of Scientific and Technical Achievements of Iranian Space Research Center Paper Presentation by: Ms. Niki Sajjad Authors: Niki Sajjad, Shahrokh Jalilian, Mehran Mirshams Paper Title: Micro satellite's ADCS simulation Date: 30 December; 2018 Place: Tehran/Iranian Space Research Center (ISRC) Symposium: 4th Specialized Meeting of Scientific and Technical Achievements of Iranian Space Research Center
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, [...]
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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 [...]
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 [...]
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. [...]
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 [...]