Journal of Space Science and Technology

Journal of Space Science and Technology

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


          

 

Keywords Cloud

  • Attitude control
  • satellite
  • Genetic Algorithm
  • optimization
  • Uncertainty
  • Reaction wheel
  • Space Radiation
  • Conceptual design
  • Remote Sensing
  • system design
  • numerical simulation
  • Satellite attitude control
  • Microgravity
  • Simulation
  • Spacecraft
  • Kalman Filter
  • Optimal control
  • Launch Vehicle
  • Multidisciplinary design optimization
  • GPS
  • Reliability
  • Optimal guidance
  • Swirl injector
  • Sounding rocket
  • Thruster
  • Reaction wheels
  • Attitude determination
  • Pitch program
  • CubeSat
  • Satellite Constellations
  • Air bearing
  • Monopropellant thruster
  • Nozzle
  • Guidance law
  • Extended Kalman Filter
  • remote sensing satellite
  • Sensitivity analysis
  • Liquid Propellant Engine
  • guidance
  • LEO satellite
  • attitude estimation
  • fault detection
  • Low thrust
  • Finite Element
  • flexible spacecraft
  • Saturation
  • INS
  • star sensor
  • Helmholtz coil
  • Star tracker
  • Inertial Navigation System
  • Outer space
  • heat transfer
  • Stability Analysis
  • Sliding mode control
  • TLE
  • Proportional navigation
  • Geostationary orbit
  • Sovereignty
  • atomization
  • Aerodynamic heating
  • manned spacecraft
  • Microstructure
  • Transverse flow
  • time series
  • State dependent riccati equation
  • Modeling
  • Star catalog
  • Reentry
  • Neural Network
  • Space Capsule
  • Spray cone
  • Fuzzy logic
  • Ground station
  • Displacement damage
  • Radiation
  • GEO satellite
  • Inertial Navigation
  • Numerical analysis
  • spacecraft formation flying
  • Solar Cell
  • Hypersonic Flow
  • Calibration
  • Magnetometer
  • vibration
  • Machine Learning
  • Electrical power subsystem
  • 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
  • Capillary injector
  • decomposition chamber
  • EKF
  • Radiation damage
  • Starlink
  • growth
  • Orbit Determination
  • simulator
  • heat flux
  • Space law
  • Combustion chamber
  • Plasma antenna
  • Stereo
  • Fault Isolation
  • 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
  • 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
  • STK software
  • TEC
  • Model predictive Control
  • Initial alignment
  • separation system
  • optimal trajectory
  • prediction
  • State control
  • Propulsion System
  • Collaborative design
  • Sloshing
  • Positioning System
  • Sun simulator
  • Thrust
  • Bipropellant propulsion system
  • redundancy
  • Primary breakup
  • Space weather
  • Asteroid Apophis
  • Space Traffic Management
  • Deep Learning
  • Launch abort system
  • Position determination
  • Flexible satellite
  • Shooting Method
  • Pulse-Width Pulse-Frequency Modulator
  • Communication satellite
  • Adaptive attitude control
  • Space industry
  • HZETRN
  • Control Allocation
  • space launch vehicle
  • breast cancer
  • linear Instability
  • Turbulent Flow
  • Optimized environment
  • 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