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