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
  • Uncertainty
  • Conceptual design
  • Space Radiation
  • Microgravity
  • Reaction wheel
  • numerical simulation
  • system design
  • Satellite attitude control
  • Remote Sensing
  • Optimal control
  • Simulation
  • Spacecraft
  • Kalman Filter
  • Launch Vehicle
  • GPS
  • Multidisciplinary design optimization
  • Attitude determination
  • Optimal guidance
  • Sounding rocket
  • Satellite Constellations
  • Swirl injector
  • Reliability
  • Extended Kalman Filter
  • Reaction wheels
  • Air bearing
  • CubeSat
  • Monopropellant thruster
  • Thruster
  • Guidance law
  • Nozzle
  • Pitch program
  • Liquid Propellant Engine
  • remote sensing satellite
  • Stability Analysis
  • TLE
  • guidance
  • Sensitivity analysis
  • Low thrust
  • Helmholtz coil
  • flexible spacecraft
  • Machine Learning
  • Inertial Navigation System
  • Star tracker
  • Saturation
  • Finite Element
  • heat transfer
  • star sensor
  • fault detection
  • attitude estimation
  • Outer space
  • Sliding mode control
  • Sun sensor
  • LEO satellite
  • INS
  • Aerodynamic heating
  • Sovereignty
  • atomization
  • manned spacecraft
  • Microstructure
  • Geostationary orbit
  • Design optimization
  • Numerical analysis
  • Magnetorquer
  • State dependent riccati equation
  • time series
  • Electrical power subsystem
  • Integrated Navigation
  • Hypersonic Flow
  • Initial alignment
  • Spray cone
  • Neural Network
  • Displacement damage
  • Space Capsule
  • Model predictive Control
  • Reentry
  • Calibration
  • Fuzzy logic
  • Positioning
  • Transverse flow
  • Solar Cell
  • Star catalog
  • Radiation
  • GEO satellite
  • 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
  • Space law
  • Numerical modeling
  • 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
  • Orbit Determination
  • Orbital maneuver
  • 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
  • Optimized environment
  • LEO Orbit
  • Space industry
  • Pulse-Width Pulse-Frequency Modulator
  • upper stage
  • HZETRN
  • Control Allocation
  • payload
  • GEANT4
  • Visual Navigation
  • space launch vehicle
  • Attitude determination and control subsystem