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