Volume 15 (2022)
Volume 14 (2021)
Volume 13 (2020)
Volume 12 (2019)
Volume 11 (2018)
Volume 10 (2017)
Volume 9 (2016)
Volume 8 (2015)
Volume 7 (2014)
Volume 6 (2013)
Volume 5 (2012)
Volume 4 (2011)
Volume 3 (2010)
Volume 2 (2009)
Volume 1 (2008)
Design and Configuration of Ground Sample Components of Low Propulsion Monopropellant Thruster Using Some Engineering Software

sajjad Davari; Hadiseh Karimaei; Mohammad Reza Salimi; Hassan Naseh

Articles in Press, Accepted Manuscript, Available Online from 21 September 2021

https://doi.org/10.30699/jsst.2021.260620.1319

Abstract
  Monopropellant thruster are used to inject a satellite into orbit or control its position on three axes in space missions. One of them is hydrazine thruster which is widely used. In this research, design of the injector, decomposition chamber and nozzle of a 10N hydrazine monopropellant thruster have ...  Read More

Space Science and Technology
Optimized Dimension Design of Catalytic Chamber of a 10 N Thruster

Hadiseh Karimaei; Hadiseh Karimaei; Mohammad Reza Salimi; Hassan Naseh

Articles in Press, Accepted Manuscript, Available Online from 21 September 2021

https://doi.org/10.30699/jsst.2021.271152.1332

Abstract
  In this paper, the catalyst bed of a 10 N hydrazine monopropellant thruster was designed. The catalyst bed is including iridium granules, which is used to decompose the hydrazine in monopropellant thruster. Hydrazine must be decomposed almost completely in the catalytic chamber, because it is a carcinogenic ...  Read More

Infrastructure (labs, sensors, software,…)
Design, Construction and Performance Evaluation of a Cold Gas Thruster Test Stand

َAlireza Alikhani; Mohammad Reza Salimi

Volume 15, Issue 1 , May 2022

https://doi.org/10.30699/jsst.2021.250452.1305

Abstract
  The cold gas thruster is one of the significant components of a satellite and its application possesses a marked impact on the entire system performance. The nonlinear function and order of magnitude, lead to increasing the importance of thruster function. Therefore, pre-mission performance assessment ...  Read More

Design of Physical Configuration of a 10N Monopropellant Hydrazine Thruster

Hadiseh Karimaei; Mohammad Reza Salimi; Hassan Naseh; Ehsan Jokari

Volume 12, Issue 1 , April 2019, , Pages 13-22

https://doi.org/10.30699/jsst.2019.1115

Abstract
  In this paper, design and physical configuration of various components of a 10N Monopropellant Hydrazine Thruster focusing on design calculations and optimization of catalytic combustion chamber. According to this design, a prototype of the thruster will be manufactured. The mentioned thruster has been ...  Read More

Performance Analysis of Liquid Propellant Micro-propulsion with Liquid Oxygen as Cryogenic Oxidizer

Amirhossein Edalatpour; Fatholah Ommi; Zoheir Saboohi

Volume 12, Issue 1 , April 2019, , Pages 23-40

https://doi.org/10.30699/jsst.2019.1121

Abstract
  Micro-propulsion Systems are low thrust engines that be used in space missions like keeping satellite in orbit and changing orbit. These engines have several kinds and liquid propellant micro-propulsion is used in this project. In two propellant micro-propulsion systems, various fuels and oxidizers can ...  Read More