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
  • system design
  • Remote Sensing
  • Microgravity
  • numerical simulation
  • Satellite attitude control
  • Simulation
  • Launch Vehicle
  • Kalman Filter
  • Spacecraft
  • Optimal control
  • GPS
  • Multidisciplinary design optimization
  • Swirl injector
  • Sounding rocket
  • Optimal guidance
  • Reliability
  • Thruster
  • Reaction wheels
  • Pitch program
  • Guidance law
  • CubeSat
  • Satellite Constellations
  • Monopropellant thruster
  • Air bearing
  • Attitude determination
  • Nozzle
  • Extended Kalman Filter
  • remote sensing satellite
  • Sensitivity analysis
  • Liquid Propellant Engine
  • guidance
  • Star tracker
  • LEO satellite
  • attitude estimation
  • Low thrust
  • flexible spacecraft
  • Saturation
  • INS
  • Helmholtz coil
  • Finite Element
  • Inertial Navigation System
  • TLE
  • 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
  • Displacement damage
  • Reentry
  • Hypersonic Flow
  • Star catalog
  • Space Capsule
  • Neural Network
  • Spray cone
  • Ground station
  • Electrical power subsystem
  • Radiation
  • Inertial Navigation
  • GEO satellite
  • Solar Cell
  • Fuzzy logic
  • 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
  • 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
  • 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
  • Pulse-Width Pulse-Frequency Modulator
  • Shooting Method
  • Adaptive attitude control
  • Reconfiguration
  • Space industry
  • HZETRN
  • Optimized environment
  • Cold gas thruster
  • space launch vehicle
  • breast cancer
  • linear Instability
  • Turbulent Flow
  • Control Allocation
  • 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