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
  • Reaction wheel
  • Space Radiation
  • Uncertainty
  • Conceptual design
  • system design
  • Microgravity
  • numerical simulation
  • Remote Sensing
  • Satellite attitude control
  • Simulation
  • Spacecraft
  • Kalman Filter
  • Launch Vehicle
  • Optimal control
  • Multidisciplinary design optimization
  • GPS
  • Swirl injector
  • Optimal guidance
  • Reliability
  • Sounding rocket
  • Thruster
  • Reaction wheels
  • Pitch program
  • Guidance law
  • CubeSat
  • Satellite Constellations
  • Extended Kalman Filter
  • Air bearing
  • Monopropellant thruster
  • Attitude determination
  • Nozzle
  • guidance
  • Sensitivity analysis
  • Liquid Propellant Engine
  • remote sensing satellite
  • Star tracker
  • LEO satellite
  • attitude estimation
  • Low thrust
  • Finite Element
  • flexible spacecraft
  • Saturation
  • INS
  • star sensor
  • Helmholtz coil
  • TLE
  • Inertial Navigation System
  • Outer space
  • fault detection
  • heat transfer
  • Stability Analysis
  • Sliding mode control
  • Proportional navigation
  • Geostationary orbit
  • Sovereignty
  • atomization
  • Aerodynamic heating
  • manned spacecraft
  • Microstructure
  • Transverse flow
  • image processing
  • 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
  • Solar Cell
  • Hypersonic Flow
  • spacecraft formation flying
  • Calibration
  • Magnetometer
  • vibration
  • Machine Learning
  • Electrical power subsystem
  • Robust Control
  • Composite
  • Sliding mode
  • launcher
  • LQR
  • Design optimization
  • Hydrogen peroxide
  • Catalyst
  • Microsatellite
  • Space
  • Terminal sliding mode
  • 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
  • Cold gas thruster
  • Fault-tolerant control
  • imaging payload
  • Communication satellite
  • Antenna Pointing Mechanism
  • 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
  • Collaborative design
  • Propulsion System
  • 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
  • Reconfiguration
  • 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