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 [...]
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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 [...]
SSS Project Constellation Initialed: in the Third Council Meeting of APSCO in September 2010; Approved: in the AOSCO council meeting as a basic activity in late 2015; Kicked-off: Dec. 12-15, 2016 in Beijing; Implementation: technical milestone meeting held, based on project schedule and implementation requirements; Launch target: first half of 2020; The SSS Constellation would have one micro-satellite (SSS-1, 30kg, 350mm * 350mm * 650mm) and two CubeSats (SSS-2A & SSS-2B, 3U, 4.0kg each), which are designed and are under manufacturing by university students from Member States under the guidance from [...]
The Summer Camp of the APSCO Student Small Satellite (SSS) Project Asia-Pacific Space Cooperation Organization (APSCO) has initiated the Student Small Satellite (SSS) project, which is aimed to train the students and faculties from Member States (MSs) of APSCO to study space technology and satellite engineering through practical design of satellites until the flight model is made, and meanwhile contribute to the development of space education systems in APSCO MSs. The ultimate goal of this project is not only to enable universities to undertake student satellite design and development, but also to impart space technologies through a satellite project [...]
Introduction for SSS project:Payload & ADCS K.N.Toosi University of Technology - The university was founded in 1928. - The university was named on behalf of K.N.Toosi the famous Persian astronomer . - It has 250 Academic staff and about 9000 students. - There are eleven faculties, 110 research & educational labs and 5 center of excellence within the university - The university is in top 10 universities of Iran. - The university is collaborating with universities from Australia, Canada, Cyprus, France, Germany, Russia, and the United Kingdom. - K.N. Toosi is one of the major R&D Partners for governmental and industrial [...]