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
  • Space Radiation
  • Uncertainty
  • Reaction wheel
  • Conceptual design
  • Satellite attitude control
  • system design
  • Microgravity
  • numerical simulation
  • Remote Sensing
  • Simulation
  • Kalman Filter
  • Spacecraft
  • Optimal control
  • Launch Vehicle
  • GPS
  • Multidisciplinary design optimization
  • Reliability
  • Swirl injector
  • Optimal guidance
  • Sounding rocket
  • Attitude determination
  • Thruster
  • Pitch program
  • Reaction wheels
  • CubeSat
  • Air bearing
  • Nozzle
  • Monopropellant thruster
  • Satellite Constellations
  • Guidance law
  • Extended Kalman Filter
  • remote sensing satellite
  • Sensitivity analysis
  • Liquid Propellant Engine
  • guidance
  • LEO satellite
  • attitude estimation
  • fault detection
  • Low thrust
  • Finite Element
  • heat transfer
  • flexible spacecraft
  • Saturation
  • star sensor
  • INS
  • Star tracker
  • Helmholtz coil
  • Inertial Navigation System
  • Outer space
  • 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
  • Neural Network
  • Star catalog
  • Reentry
  • Spray cone
  • Solar Cell
  • Fuzzy logic
  • Ground station
  • Displacement damage
  • Radiation
  • GEO satellite
  • Inertial Navigation
  • Modeling
  • Numerical analysis
  • spacecraft formation flying
  • Space Capsule
  • 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
  • Space law
  • 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
  • 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
  • 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
  • State control
  • Propulsion System
  • Collaborative design
  • Sloshing
  • Positioning System
  • Sun simulator
  • redundancy
  • Bipropellant propulsion system
  • Primary breakup
  • Space weather
  • Deep Learning
  • Asteroid Apophis
  • Launch abort system
  • STK software
  • Space Traffic Management
  • Position determination
  • Flexible satellite
  • Shooting Method
  • Adaptive attitude control
  • Communication satellite
  • Space industry
  • Pulse-Width Pulse-Frequency Modulator
  • HZETRN
  • Control Allocation
  • space launch vehicle
  • breast cancer
  • linear Instability
  • Turbulent Flow
  • Attitude determination and control subsystem
  • LEO Orbit
  • Nonlinear Quadratic Tracking (NQT)
  • space structures
  • Optimized environment
  • CanSat
  • Integrated Navigation
  • Magnetic field
  • sensitivity matrix
  • Hardware in the loop
  • Differential flatness
  • PSO optimization