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
  • Conceptual design
  • Space Radiation
  • Microgravity
  • Satellite attitude control
  • system design
  • Remote Sensing
  • numerical simulation
  • Spacecraft
  • Kalman Filter
  • Launch Vehicle
  • Optimal control
  • Simulation
  • GPS
  • Multidisciplinary design optimization
  • Sounding rocket
  • Optimal guidance
  • Reliability
  • Swirl injector
  • Nozzle
  • Reaction wheels
  • Air bearing
  • Satellite Constellations
  • CubeSat
  • Attitude determination
  • Thruster
  • Monopropellant thruster
  • Extended Kalman Filter
  • Pitch program
  • Guidance law
  • Sensitivity analysis
  • guidance
  • LEO satellite
  • fault detection
  • attitude estimation
  • Liquid Propellant Engine
  • Star tracker
  • Finite Element
  • Helmholtz coil
  • heat transfer
  • remote sensing satellite
  • Saturation
  • star sensor
  • TLE
  • flexible spacecraft
  • INS
  • 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
  • Spray cone
  • Reentry
  • Space Capsule
  • Electrical power subsystem
  • Neural Network
  • Hypersonic Flow
  • Composite
  • Ground station
  • Modeling
  • Numerical analysis
  • GEO satellite
  • Inertial Navigation
  • Calibration
  • Star catalog
  • Fuzzy logic
  • Solar Cell
  • time series
  • Magnetometer
  • spacecraft formation flying
  • Machine Learning
  • vibration
  • LQR
  • Displacement damage
  • 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
  • Orbit Determination
  • Starlink
  • Radiation damage
  • Fault Isolation
  • Combustion chamber
  • Numerical modeling
  • Space law
  • growth
  • simulator
  • Plasma antenna
  • Stereo
  • 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
  • Antenna Pointing Mechanism
  • Reconfiguration
  • Uncertainty and actuator saturation
  • Gyro calibration
  • gimbal control moment gyro
  • Positioning
  • LEO
  • 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
  • Space Traffic Management
  • Position determination
  • Deep Learning
  • Shooting Method
  • Launch abort system
  • Communication satellite
  • Flexible satellite
  • Pulse-Width Pulse-Frequency Modulator
  • Adaptive attitude control
  • Space industry
  • breast cancer
  • HZETRN
  • linear Instability
  • Turbulent Flow
  • Control Allocation
  • Satellite remote sensing
  • space launch vehicle
  • Attitude determination and control subsystem
  • Nonlinear Quadratic Tracking (NQT)
  • CanSat
  • space structures
  • Magnetic field
  • Optimized environment
  • Integrated Navigation
  • sensitivity matrix
  • Hardware in the loop