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

 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
  • Uncertainty
  • Reaction wheel
  • Microgravity
  • numerical simulation
  • Satellite attitude control
  • Remote Sensing
  • system design
  • Spacecraft
  • Launch Vehicle
  • Simulation
  • Optimal control
  • Kalman Filter
  • Multidisciplinary design optimization
  • GPS
  • Satellite Constellations
  • Swirl injector
  • Reliability
  • Optimal guidance
  • Sounding rocket
  • Guidance law
  • Reaction wheels
  • CubeSat
  • Monopropellant thruster
  • Air bearing
  • Nozzle
  • Thruster
  • Extended Kalman Filter
  • Attitude determination
  • Pitch program
  • guidance
  • Sensitivity analysis
  • Liquid Propellant Engine
  • remote sensing satellite
  • TLE
  • Star tracker
  • attitude estimation
  • Low thrust
  • fault detection
  • Finite Element
  • Helmholtz coil
  • Saturation
  • heat transfer
  • star sensor
  • Stability Analysis
  • LEO satellite
  • INS
  • Outer space
  • flexible spacecraft
  • Sliding mode control
  • Inertial Navigation System
  • Proportional navigation
  • Sovereignty
  • Aerodynamic heating
  • atomization
  • manned spacecraft
  • Microstructure
  • Geostationary orbit
  • Terminal sliding mode
  • Numerical analysis
  • Calibration
  • Fuzzy logic
  • Hypersonic Flow
  • Star catalog
  • Space Capsule
  • Neural Network
  • Reentry
  • GEO satellite
  • Transverse flow
  • Inertial Navigation
  • Radiation
  • Modeling
  • Ground station
  • Displacement damage
  • time series
  • Spray cone
  • Solar Cell
  • Magnetometer
  • spacecraft formation flying
  • Machine Learning
  • vibration
  • LQR
  • Composite
  • launcher
  • State dependent riccati equation
  • Sliding mode
  • Design optimization
  • Catalyst
  • Robust Control
  • image processing
  • Space
  • Hydrogen peroxide
  • Microsatellite
  • Magnetorquer
  • Electrical power subsystem
  • cryogenic
  • Artificial Neural Networks
  • Space law
  • heat flux
  • Responsibility
  • design algorithm
  • IMU
  • orbital mechanics
  • decomposition chamber
  • Solid Rocket Motor
  • EKF
  • Orbit Determination
  • Fault Isolation
  • Starlink
  • Radiation damage
  • Capillary injector
  • growth
  • Artificial Neural Network
  • Combustion chamber
  • Stereo
  • design requirements
  • Numerical modeling
  • Orbital maneuver
  • Plasma antenna
  • simulator
  • 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
  • HZETRN
  • linear Instability
  • Recursive least squares
  • Satellite remote sensing
  • Attitude determination and control subsystem
  • space launch vehicle
  • Differential flatness
  • upper stage
  • Optimized environment
  • payload
  • space structures
  • Visual Navigation
  • implicit guidance
  • Hardware in the loop