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