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