Space subsystems design: (navigation, control, structure and…)
Design for reliability of a space system in the conceptual design phase

hamid reza ali mohamadi; Hassan Naseh

Articles in Press, Accepted Manuscript, Available Online from 25 September 2023

Abstract
  Achieving to new technologies with high reliability, along with reducing the cost and time of the design cycle, is one of the most important challenges in complex systems. In this paper, reliability based design of a space system is discussed in the conceptual design phase. Normally, there are eight ...  Read More

Space systems design (spacecraft, satellites, space stations and their equipment)
Design, fabrication, and test of a cryogenic liquid oxygen-ethanol engine

Hojat Ghasemi; Seyed Mohammadreza Mahmoudian; Noordin Qadiri Massoom; S. Rashad Rouholamini; Pouria Mikaniki; Asghar Azimi

Volume 16, Issue 1 , March 2023, , Pages 47-58

Abstract
  The aim of the present research is to obtain the ability to use the cryogenic propellant engines on a laboratory scale. In this regard, it is necessary to build some experimental motors and investigate the their performance parameters. The liquid oxygen as a common oxidizer and ethanol as a green fuel ...  Read More

Comprehensive Pattern in Designing Low-Thrust Space Propulsion Systems

H. Fazeli; H. Naseh; M. Mirshams; A.B. Novinzadeh

Volume 7, Issue 3 , October 2014, , Pages 9-21

Abstract
  Designing space propulsion systems as one of the important subsystems of the spacecrafts and upper stage space launch systems needs to bypass different and complicated steps. In this article the comprehensive process of designing liquid fuel low-thrust space propulsion systems was illustrated. In the ...  Read More

Neural Network Based Diagnostic Indication of a Liquid Propellant Engine with Faulty Data Collection System

S. Khodadadiyan; R. Farokhi; D. Ramesh

Volume 7, Issue 2 , July 2014, , Pages 75-83

Abstract
  The aim of the paper is to describe a methodology of damage detection in the liquid propellant engine which is based on artificial neural networks in combination with stochastic analysis. It is assumed that the liquid propellant engine have faulty data collection system. Then a filtering algorithm for ...  Read More