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