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

 ARI, 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 2, 2026, Pages 1-69 

Keywords Cloud

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