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