Journal of Space Science and Technology

Journal of Space Science and Technology

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

ARI, IAS

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


          

 

Current Issue: Volume 19, Issue 3, 2026 

Machine Learning–Driven Prediction of the S4 Scintillation Index and Geomagnetic Storms using GNSS-RO Data

Pages 13-29

10.22034/jsst.2025.1585

Delaram Fattahi, Sahar Barzegar, Masoud Khoshsima, Saber Karami, Hadi Jalili, Jamal Aghayari

Keywords Cloud

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