Journal of Space Science and Technology

Journal of Space Science and Technology

Journal of Space Science and Technology

Journal Archive

Journal of Space Science and Technology is an open access double-blind peer-reviewed quarterly journal, owned, managed and published by IAS since 2008. The journal publishes original and high-quality peer-reviewed papers containing significant results relevant to all aspects of Space System Engineering, Space Operation and Applications, Commerce, Management, Space Law, Space Sciences and Exploration and Investigating Space Radiation.

Journal Title

 Journal of Space Science and Technology

P-ISSN

 2008-4560

E-ISSN

 2423-4516

Frequency

 Quarterly

Editor-in-Chief

 Reza Ebrahimi, Ph.D.

Language 

 Persian with English Abstracts

Plagiarism Checker

 Hamanandjo, iThenticate

Peer Review Policy

 Double-blind

Article Processing Charges

 No APC (Free)

Average Review Time

 3 Months

Acceptance Rate

 30%

Owner & Publisher

 IAS

The Journal of Space Science and Technology is now accepting original research papers in English also featuring a swift review prosses

          

 

Most Visited Articles
Physical Initial Flight Alignment for Stabilized Platform Inertial Navigation System Using State Feedback
Free Vibration Analysis of Grid Stiffened Doubly Curved Composite Shells Using a Refined Higher Order Theory
Scientometric Analysis of Published Scientific Productions in the Field of Satellite Constellations
A Review on Underactuated Attitude Control of Reaction Wheel Actuated Satellites
Research Trends in Utilizing Artificial Intelligence in Satellite-Based Internet of Things: A Scientometric Analysis
GPS-RTK Integrated with Micro-Electro Mechanical INS for Precise Application
Performance Analysis of FMC Actuators to Microsatellite Temperature Management Based on 3-Axis and Pyramidal Configuration
Current Issue: Volume 19, Issue 1, 2026 

Original Research Paper

Preliminary Design of a Single-Unit CubeSat for a Earthquake Prediction Mission

Pages 1-19

10.22034/jsst.2025.1554

Abolghasem Naghash, Mohammad Reza Zeinoldini, Javad Salemi, Mohammad Abri, Narges Nikbakht, Seyed Yousoof Hosseini Akhgar, Mohammad Hassn Hashemzadeh

Keywords Cloud

  • Attitude control
  • satellite
  • Genetic Algorithm
  • optimization
  • Space Radiation
  • Conceptual design
  • Reaction wheel
  • Uncertainty
  • system design
  • Microgravity
  • Remote Sensing
  • numerical simulation
  • Satellite attitude control
  • Optimal control
  • Kalman Filter
  • Launch Vehicle
  • Simulation
  • Spacecraft
  • Multidisciplinary design optimization
  • GPS
  • Swirl injector
  • Optimal guidance
  • Sounding rocket
  • Reliability
  • Thruster
  • Reaction wheels
  • Pitch program
  • Guidance law
  • CubeSat
  • Satellite Constellations
  • Air bearing
  • Monopropellant thruster
  • Extended Kalman Filter
  • Attitude determination
  • Nozzle
  • remote sensing satellite
  • Sensitivity analysis
  • guidance
  • LEO satellite
  • attitude estimation
  • Low thrust
  • Liquid Propellant Engine
  • Finite Element
  • flexible spacecraft
  • Saturation
  • INS
  • star sensor
  • Helmholtz coil
  • TLE
  • Star tracker
  • Inertial Navigation System
  • Outer space
  • fault detection
  • heat transfer
  • Stability Analysis
  • Sliding mode control
  • Proportional navigation
  • Geostationary orbit
  • Sovereignty
  • atomization
  • Aerodynamic heating
  • manned spacecraft
  • Microstructure
  • Transverse flow
  • image processing
  • time series
  • State dependent riccati equation
  • Modeling
  • Reentry
  • Hypersonic Flow
  • Star catalog
  • Space Capsule
  • Neural Network
  • Spray cone
  • Ground station
  • Displacement damage
  • Radiation
  • Inertial Navigation
  • GEO satellite
  • Numerical analysis
  • Solar Cell
  • Fuzzy logic
  • spacecraft formation flying
  • Calibration
  • Magnetometer
  • vibration
  • Machine Learning
  • Electrical power subsystem
  • Robust Control
  • Composite
  • Sliding mode
  • launcher
  • LQR
  • Design optimization
  • Hydrogen peroxide
  • Catalyst
  • Microsatellite
  • Space
  • Terminal sliding mode
  • Artificial Neural Networks
  • cryogenic
  • Space law
  • design requirements
  • Numerical modeling
  • injection
  • Artificial Neural Network
  • design algorithm
  • Responsibility
  • decomposition chamber
  • orbital mechanics
  • IMU
  • Sandwich panels
  • Capillary injector
  • EKF
  • Radiation damage
  • Starlink
  • growth
  • Orbit Determination
  • simulator
  • heat flux
  • Combustion chamber
  • Orbital maneuver
  • Plasma antenna
  • Stereo
  • Fault Isolation
  • UDF
  • Nanosatellite
  • Required velocity
  • Quantitative feedback theory
  • Visual Navigation
  • payload
  • GEANT4
  • upper stage
  • Satellite subsystems
  • Thrust vector control
  • Monopropellant
  • Cost
  • Solid Rocket Motor
  • Satellite remote sensing
  • Recursive least squares
  • thermal control
  • solar array
  • Cold gas thruster
  • Fault-tolerant control
  • imaging payload
  • Communication satellite
  • Antenna Pointing Mechanism
  • Uncertainty and actuator saturation
  • Gyro calibration
  • gimbal control moment gyro
  • Positioning
  • LEO
  • Non-interfering architecture
  • STK software
  • TEC
  • Model predictive Control
  • Initial alignment
  • separation system
  • optimal trajectory
  • prediction
  • State control
  • Propulsion System
  • Positioning System
  • Deep Learning
  • Sun simulator
  • Sloshing
  • Collaborative design
  • Bipropellant propulsion system
  • redundancy
  • Primary breakup
  • Space weather
  • Asteroid Apophis
  • Space Traffic Management
  • Thrust
  • Launch abort system
  • Position determination
  • Flexible satellite
  • Shooting Method
  • Pulse-Width Pulse-Frequency Modulator
  • Reconfiguration
  • Adaptive attitude control
  • Space industry
  • HZETRN
  • Optimized environment
  • space launch vehicle
  • breast cancer
  • linear Instability
  • Turbulent Flow
  • Control Allocation
  • LEO Orbit
  • Nonlinear Quadratic Tracking (NQT)
  • space structures
  • Differential flatness
  • CanSat
  • Integrated Navigation
  • Magnetic field
  • Attitude determination and control subsystem
  • Hardware in the loop
  • sensitivity matrix
  • PSO optimization