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)
Provide a Predictive Model for the Preliminary Design of Swirl Injectors Based on Neuro-Fuzzy Model

Hadiseh Karimaei

Volume 12, Issue 2 , September 2019, , Pages 11-21

https://doi.org/10.30699/jsst.2019.81952

Abstract
  the effect of the internal geometry of the injector of a low-thrust monopropellant thruster on the characteristics of the outlet liquid sheet, such as the liquid sheet thickness, the spray cone angle, the average output velocity, and its mass flow rate, have been studied. For this purpose, simulation ...  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

Design and Simulation of Fuel Injector of a 10N Monopropellant Hydrazine Thruster

Hadiseh Karimaei

Volume 11, Issue 3 , December 2018, , Pages 9-19

Abstract
  Monopropellant thruster of atitude control system is a requirement for the development and functionalization of satellites in space, which have expensive and high-tech technology. Hydrazine thrusters are currently the most widely used thrusters for guidance and control systems of re-entry and manned ...  Read More

Microscopic Test of a Swirl Injector by High-speed Photography

Hadiseh Karimaei; Mostafa Hossein Alipour; F Ommi; Ehsan Movahednejad; Reza Sharifzadeh

Volume 10, Issue 4 , March 2018, , Pages 1-7

Abstract
  A swirl injector is tested to investigate the instability of the liquid sheet emanating from it and determine the main microscopic characteristics of the spray. The injector, which is tested, was already approved by doing the characterization tests (macroscopic). Due to the fact that the PDPA systems ...  Read More

Extraction of a Theoretical Energy-based Model to Estimate Mean Droplet Diameter of the Swirl Injector Spray

Hadiseh Karimaei; seyed mostafa hosseinalipour

Volume 10, Issue 3 , December 2017, , Pages 59-65

Abstract
  The droplet formation stage of a spray, which enjoys a great diversity in size and droplet velocity, is predictable through a statistical approach. Since the available methods require experimental data such as mean droplet diameter and mean droplet velocity as inputs to estimate the distribution of the ...  Read More

Review of a Swirl Double Base Injector Performance by It’s Hot-Fire Test on a Laboratory Liquid Micro Impulse Engine With Single Injector

Saeedeh Ya’ghob-nezhad; Seyed Hamed Hashemi Mehne

Volume 9, Issue 1 , May 2016, , Pages 73-89

Abstract
  Because of vast applications of Liquid fuel engines in rockets and importance of their functional parameters such as trust, specific impulse and fuel consumption in engine performance, it is needed to be tested in different functional conditions before operation in actual missions. The analysis of test ...  Read More