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
  • Space Radiation
  • Reaction wheel
  • Conceptual design
  • Satellite attitude control
  • numerical simulation
  • Remote Sensing
  • system design
  • Microgravity
  • Spacecraft
  • Kalman Filter
  • Optimal control
  • Simulation
  • Launch Vehicle
  • 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
  • Saturation
  • TLE
  • INS
  • flexible spacecraft
  • star sensor
  • Inertial Navigation System
  • 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
  • Fuzzy logic
  • Hypersonic Flow
  • Solar Cell
  • Space Capsule
  • Displacement damage
  • Neural Network
  • Composite
  • Ground station
  • Modeling
  • Numerical analysis
  • Inertial Navigation
  • GEO satellite
  • Calibration
  • time series
  • Star catalog
  • Spray cone
  • spacecraft formation flying
  • Reentry
  • Machine Learning
  • vibration
  • LQR
  • Magnetometer
  • 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
  • Numerical modeling
  • Artificial Neural Network
  • design requirements
  • Orbital maneuver
  • design algorithm
  • IMU
  • Responsibility
  • decomposition chamber
  • EKF
  • Solid Rocket Motor
  • orbital mechanics
  • injection
  • Starlink
  • Radiation damage
  • Capillary injector
  • growth
  • Orbit Determination
  • heat flux
  • simulator
  • 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
  • Cold gas thruster
  • Fault-tolerant control
  • imaging payload
  • Uncertainty and actuator saturation
  • Antenna Pointing Mechanism
  • LEO
  • Gyro calibration
  • Launch abort system
  • gimbal control moment gyro
  • Positioning
  • Non-interfering architecture
  • STK software
  • TEC
  • Model predictive Control
  • Initial alignment
  • separation system
  • optimal trajectory
  • prediction
  • State control
  • Propulsion System
  • Positioning System
  • Deep Learning
  • Collaborative design
  • Bipropellant propulsion system
  • Sun simulator
  • Sloshing
  • redundancy
  • Asteroid Apophis
  • Space Traffic Management
  • Primary breakup
  • Space weather
  • Position determination
  • Thrust
  • Shooting Method
  • Flexible satellite
  • Reconfiguration
  • Pulse-Width Pulse-Frequency Modulator
  • Adaptive attitude control
  • Space industry
  • Communication satellite
  • breast cancer
  • HZETRN
  • linear Instability
  • Turbulent Flow
  • Optimized environment
  • Satellite remote sensing
  • Attitude determination and control subsystem
  • Control Allocation
  • Nonlinear Quadratic Tracking (NQT)
  • CanSat
  • Integrated Navigation
  • Magnetic field
  • space structures
  • PSO optimization
  • sensitivity matrix
  • Hardware in the loop