Volume 16 (2023)
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)
Number of Volumes 17
Number of Issues 60
Number of Articles 452
Number of Contributors 814
Article View 319,307
PDF Download 173,512
View Per Article 706.43
PDF Download Per Article 383.88
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Number of Submissions 857
Acceptance Rate 49
Time to Accept (Days) 156
Number of Indexing Databases 15
Number of Reviewers 726

Journal of Space Science and Technology (JSST), is an open access double blind peer reviewed quarterly publication which is published by  Aerospace Research Institute and publishes high quality papers on all aspects of Space System Engineering, Space operation and applications, commerce, management, and Space law, Space Sciences and Exploration and Investigating Space Radiation. The following manuscript format can be published in the journal: Original article, short communication (brief report or brief communication), review article, systematic review and meta-analysis, Letter to editor, commentary, and editorial in journal scopes.

Publication Fee: article processing charge and any other publication fees in the journal space science and technology are free for authors.
Subscription Fee: Journal of Space Science is no subscription fee for audiences.

review time is a maximum three months from receipt to acceptance.   

bibliography method: IEEE , EndNote 

Space Science and Technology also a member of the Committee on Publication Ethics (COPE).

All submitted manuscripts are checked for similarity through a trustworthy software named Hamanandjo software to be assured about its originality and then rigorously peer-reviewed by the international reviewers.

Space Science and Technology is licensed under a " Creative Commons Attribution License (CC BY)

Having an ORCID identifier is mandatory for all authors. You can register at https://orcid.org/register.

      


 

Research Paper GPS and navigation GPS)، GLONASS، GALILEO
Physical Initial Flight Alignment For Stabilized Platform Inertial Navigation system Using State Feedback

Seyed Ali Zahiripour

Volume 17, Issue 1 , March 2024, Pages 1-9

Abstract
  A method for increasing the accuracy of the initial alignment process of inertial navigation systems with a stable platform is presented through state feedback control in flight mode. In the presented method, the state feedback controller is designed by using the stable plate deviation angles and the ...  Read More

Research Paper Space subsystems design: (navigation, control, structure and…)
Development of an EKF Based Gyro Calibration Method for High-Precision Attitude Estimation

Amir Labibian

Volume 17, Issue 1 , March 2024, Pages 11-20

Abstract
  IIn high resolution remote sensing satellites, meeting stability and pointing requirements are very crucial in mission’s success. In this regard, usually, very accurate gyroscopes are utilized as one of the main attitude sensors. In order to avoid decreasing attitude estimation accuracies, gyroscopes ...  Read More

Research Paper GPS and navigation GPS)، GLONASS، GALILEO
Efficiency of the least squares support vector regression in local modeling of the ionosphere total electron content and comparison with other models

Tania Mansour Fallah; Behzad Voosoghi; Seyyed Reza Ghaffari-Razin

Volume 17, Issue 1 , March 2024, Pages 21-36

Abstract
  In this paper, the aim is to use the least squares support vector regression (LS-SVR) for spatio-temporal modeling of the ionospheric total electron content (TEC). In order to do this, the observations of 15 GPS stations in the north-west of Iran have been used in the period from 193 to 228 at 2012. ...  Read More

Research Paper communications
Optimizing and increasing the reliability in high power supply using TWTA lamps

Peyman Mohammadi; Mehdi Alemi Rostami

Volume 17, Issue 1 , March 2024, Pages 37-48

Abstract
  One of the most important issues related to the power supply of TWTA lamps in satellites is to have low ripple, high efficiency, high reliability and optimal volume and weight,. In this article, the efficiency and reliability of high voltage DC/DC electronic-power converter is optimized for use in satellite ...  Read More

Research Paper space policy
Explaining the Development Strategy of Space Technology Based on the Developing Models of Countries

Hadi Jalili

Volume 17, Issue 1 , March 2024, Pages 49-62

Abstract
  In this paper, the models of space technology development in regional countries have been studied first, and the main criteria of each of these models have been classified. In this research, by ignoring the leading countries such as USA, Russia, European Union, China, Japan and India, the prominent countries ...  Read More

Research Paper physiology and space medicine (astrobiology)
Cadmium bioremoval from water by probiotics in simulated microgravity and Mars gravity

maryam salavatifar

Volume 17, Issue 1 , March 2024, Pages 63-71

Abstract
  Earth's gravity is one of the forces that constantly affects living organisms. It's changes can affect organisms behavior and performance. Study of such effects can lead to the discovery of new practical methods. Heavy metal toxicity have a lot of risks to human health. They sometimes act as a pseudo ...  Read More

Research Paper Space subsystems design: (navigation, control, structure and…)
Design and Fabrication of Planar Sub-Array for Satellite Data Transmission Directive Conformal Array Antenna

Arian Zakiani; Seyed Hassan Sedighy; Razieh Narimani

Volume 17, Issue 1 , March 2024, Pages 73-79

Abstract
  Due to the limited communication time between LEO satellites and the ground station and large volume of satellite image data, it is necessary to establish a high transmission rate connection. Therefore, the use of a high-efficiency satellite antenna is inevitable. In order to use the limited viewing ...  Read More

GPS and navigation GPS)، GLONASS، GALILEO
Physical Initial Flight Alignment For Stabilized Platform Inertial Navigation system Using State Feedback

Seyed Ali Zahiripour

Volume 17, Issue 1 , March 2024, , Pages 1-9

Abstract
  A method for increasing the accuracy of the initial alignment process of inertial navigation systems with a stable platform is presented through state feedback control in flight mode. In the presented method, the state feedback controller is designed by using the stable plate deviation angles and the ...  Read More

Space New Technologies
A Review of the Applications of Artificial Intelligence in Improving the Performance of Integrated Space-Air and Ground Networks

Pedram Hajipour; Roghieh Karimzadeh Baee; Houman Zarrabi; Roghayeh Doost; Leila Mohammadi

Volume 16, Issue 2 , June 2023, , Pages 27-42

Abstract
  According to the technical specifications of the future generations of telecommunication (the fifth generation and later), which should provide new services with very high data rates in the minimum time and a wide coverage, as well as the exponential increase in traffic, the use of combined space-air ...  Read More

Space subsystems design: (navigation, control, structure and…)
Attitude and Vibration Control of a Flexible Spacecraft Using Hybrid Adaptive Super-Twisting Non-Singular Terminal Sliding Mode Control

Valiollah Shahbahrami; Milad َAzimi; َAlireza Alikhani

Volume 16, Issue 4 , December 2023, , Pages 1-13

Abstract
  In this paper, a robust adaptive hybrid control approach based on a combination of super-twisting and non-singular terminal sliding mode control (STNSMC) approaches for vibration and attitude control of a flexible spacecraft with fully coupled dynamic is developed. The proposed adaptation law eliminates ...  Read More

Space systems design (spacecraft, satellites, space stations and their equipment)
Optimized Dimension Design of Catalytic Chamber of a 10 N Thruster

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

Volume 16, Issue 2 , June 2023, , Pages 55-61

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

Space subsystems design: (navigation, control, structure and…)
Adaptive Generalized-Minimum-Variance Attitude Control of a High Pointing-Accuracy Remote Sensing Satellite

Ali Kasiri; Farhad Fani Saberi; Vahid Joudakian

Volume 16, English Special Issue , November 2023, , Pages 1-23

Abstract
  Many studies have investigated the problem of external disturbance rejection and also increasing the attitude control system's robustness against the parametric uncertainties. Due to stochastic properties, noise effect minimization becomes an interesting and challenging problem in the field of spacecraft ...  Read More

Research Paper space sciences and exploration
Spacecraft Trajectory Design Regarding Van Allen Belts by Honey Bee Optimisation Algorithm

Iman Shafieenejad

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

Abstract
  The aim of this research is to optimize the trajectory of a low-trust spacecraft carrying biological cargo. Reducing the radiation stresses of the Van Allen belt is the optimal criterion of the optimal control problem of the orbital transfer from the low orbits to the high orbits. Since the minimum radiation ...  Read More

Research Paper communications
A Reconfigurable and Steerable Horn Antenna Using Plasma Dielectric Slabs for Controllable Gain and Beam Steering

Jaafar Bazrafshan; Fatemeh Sadeghikia; Ali Karami Horestani; Mohamed Himdi

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

Abstract
  This paper presents a novel approach for designing a reconfigurable and steerable antenna utilizing plasma dielectric slabs along the aperture of a pyramidal horn antenna. The antenna offers electronic control over both the radiation gain and the direction of the main beam. The proposed configuration ...  Read More

Research Paper 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

Research Paper space sciences and exploration
Economic analysis of exploitation of lunar resources

Ebrahim Amiri; Masoome Khani Chamani; Mahdi Jafari-Nodoshan; Sajjad Ghazanfarinia; Masoud Khoshsima

Articles in Press, Accepted Manuscript, Available Online from 16 December 2023

Abstract
  The economic model generally expresses the mechanisms used to earn money from a business, and if it doesnot generate income, its failure will be certain. Therefore, the decision to carry out a mission isnot only based on technical specifications, and besides that, economic profitability is another part ...  Read More

Research Paper cellular-molecular biology
E-cadherin gene expression changes in MCF-7 breast cancer cell line in simulated microgravity condition

Zahra Hajebrahimi

Articles in Press, Accepted Manuscript, Available Online from 30 December 2023

Abstract
  Simulated microgravity can change tumor cell adhesion, proliferation, invasion, and metastasis. E-cadherin molecule is a cell-to-cell adhesion regulatory molecule whose expression is reduced in most types of cancer cells. In the present study, the expression of the E-cadherin gene in the MCF-7 breast ...  Read More

Research Paper Space systems design (spacecraft, satellites, space stations and their equipment)
Investigation the effect of flameholder on the combustion chamber performance of a ramjet engine

Sajjad Gharezi; Mohammad Mehdi Doustdar

Articles in Press, Accepted Manuscript, Available Online from 17 January 2024

Abstract
  In this research, the design of a can combustion chamber for a ramjet engine, the performance of this chamber and the role of flameholder have been studied. For this purpose, after talking about ramjet engine types, some general information about the combustion chamber has been explained. Then the process ...  Read More

Review Paper communications
Scientometric analysis of published scientific productions in the field of satellite constellations

Pedram Hajipour; Hossein Eftekhari; Ali Kheirdoost; Hassan Yeganeh

Articles in Press, Accepted Manuscript, Available Online from 03 March 2024

Abstract
  Satellite constellations include a set of similar satellites that are distributed in a specific orbital pattern to accomplish a common mission. Satellite constellations are commonly used to accomplish missions such as global telecommunications, global positioning, and remote sensing. In this article, ...  Read More

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