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
  • Conceptual design
  • Reaction wheel
  • Uncertainty
  • Space Radiation
  • Satellite attitude control
  • Remote Sensing
  • Microgravity
  • numerical simulation
  • system design
  • Kalman Filter
  • Simulation
  • Launch Vehicle
  • Spacecraft
  • Optimal control
  • Multidisciplinary design optimization
  • GPS
  • Satellite Constellations
  • Swirl injector
  • Reliability
  • Optimal guidance
  • Sounding rocket
  • Guidance law
  • Reaction wheels
  • Extended Kalman Filter
  • Monopropellant thruster
  • Air bearing
  • Nozzle
  • Thruster
  • CubeSat
  • Attitude determination
  • Pitch program
  • guidance
  • Sensitivity analysis
  • remote sensing satellite
  • TLE
  • Star tracker
  • Low thrust
  • fault detection
  • Liquid Propellant Engine
  • Finite Element
  • Helmholtz coil
  • Inertial Navigation System
  • heat transfer
  • star sensor
  • LEO satellite
  • Stability Analysis
  • INS
  • Outer space
  • flexible spacecraft
  • Sliding mode control
  • attitude estimation
  • Saturation
  • Proportional navigation
  • Aerodynamic heating
  • atomization
  • manned spacecraft
  • Microstructure
  • Geostationary orbit
  • Sovereignty
  • Terminal sliding mode
  • Numerical analysis
  • Calibration
  • Fuzzy logic
  • Hypersonic Flow
  • Star catalog
  • Space Capsule
  • Neural Network
  • Reentry
  • GEO satellite
  • Transverse flow
  • Modeling
  • Inertial Navigation
  • Radiation
  • 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
  • Artificial Neural Network
  • Orbital maneuver
  • design algorithm
  • IMU
  • orbital mechanics
  • decomposition chamber
  • Solid Rocket Motor
  • EKF
  • Responsibility
  • Orbit Determination
  • Fault Isolation
  • Capillary injector
  • Radiation damage
  • Starlink
  • growth
  • Combustion chamber
  • design requirements
  • Numerical modeling
  • Stereo
  • 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
  • Communication satellite
  • Positioning
  • Reconfiguration
  • Shooting Method
  • Space Traffic Management
  • Position determination
  • Gyro calibration
  • Uncertainty and actuator saturation
  • 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
  • Space industry
  • Adaptive attitude control
  • Antenna Pointing Mechanism
  • LEO
  • Pulse-Width Pulse-Frequency Modulator
  • Fault-tolerant control
  • Control Allocation
  • Optimized environment
  • linear Instability
  • Recursive least squares
  • Satellite remote sensing
  • HZETRN
  • space launch vehicle
  • Differential flatness
  • upper stage
  • sensitivity matrix
  • payload
  • space structures
  • Visual Navigation
  • Attitude determination and control subsystem
  • Hardware in the loop