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
  • Conceptual design
  • Reaction wheel
  • Uncertainty
  • Space Radiation
  • Remote Sensing
  • numerical simulation
  • Microgravity
  • system design
  • Satellite attitude control
  • Optimal control
  • Kalman Filter
  • Spacecraft
  • Simulation
  • Launch Vehicle
  • Multidisciplinary design optimization
  • GPS
  • Swirl injector
  • Optimal guidance
  • Reliability
  • Sounding rocket
  • Thruster
  • Reaction wheels
  • Pitch program
  • Guidance law
  • CubeSat
  • Satellite Constellations
  • Monopropellant thruster
  • Air bearing
  • Attitude determination
  • Extended Kalman Filter
  • Nozzle
  • remote sensing satellite
  • Sensitivity analysis
  • guidance
  • LEO satellite
  • attitude estimation
  • Low thrust
  • Liquid Propellant Engine
  • flexible spacecraft
  • Saturation
  • INS
  • Helmholtz coil
  • Finite Element
  • Inertial Navigation System
  • TLE
  • Star tracker
  • 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
  • GEO satellite
  • Inertial Navigation
  • 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
  • design requirements
  • Numerical modeling
  • injection
  • Artificial Neural Network
  • design algorithm
  • Responsibility
  • decomposition chamber
  • orbital mechanics
  • IMU
  • Sandwich panels
  • Capillary injector
  • EKF
  • Radiation damage
  • Starlink
  • growth
  • Orbit Determination
  • simulator
  • heat flux
  • Combustion chamber
  • Orbital maneuver
  • 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
  • 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
  • Control Allocation
  • Cold gas thruster
  • 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