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
  • Conceptual design
  • Space Radiation
  • system design
  • numerical simulation
  • Microgravity
  • Satellite attitude control
  • Remote Sensing
  • Simulation
  • Kalman Filter
  • Optimal control
  • Spacecraft
  • Launch Vehicle
  • GPS
  • Multidisciplinary design optimization
  • Reliability
  • Sounding rocket
  • Optimal guidance
  • Swirl injector
  • 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
  • star sensor
  • attitude estimation
  • fault detection
  • Low thrust
  • Finite Element
  • heat transfer
  • flexible spacecraft
  • Saturation
  • INS
  • LEO satellite
  • Star tracker
  • Helmholtz coil
  • Outer space
  • Inertial Navigation System
  • Stability Analysis
  • Sliding mode control
  • TLE
  • Proportional navigation
  • Geostationary orbit
  • Sovereignty
  • atomization
  • Aerodynamic heating
  • manned spacecraft
  • Microstructure
  • Transverse flow
  • State dependent riccati equation
  • Modeling
  • Star catalog
  • Reentry
  • Hypersonic Flow
  • Neural Network
  • Displacement damage
  • Spray cone
  • Solar Cell
  • Ground station
  • Electrical power subsystem
  • Radiation
  • Inertial Navigation
  • GEO satellite
  • Numerical analysis
  • time series
  • Space Capsule
  • Fuzzy logic
  • Calibration
  • Magnetometer
  • vibration
  • Machine Learning
  • spacecraft formation flying
  • 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
  • Communication satellite
  • Fault-tolerant control
  • imaging payload
  • Uncertainty and actuator saturation
  • Antenna Pointing Mechanism
  • LEO
  • Gyro calibration
  • Space Traffic Management
  • gimbal control moment gyro
  • Positioning
  • Non-interfering architecture
  • Model predictive Control
  • TEC
  • prediction
  • Initial alignment
  • Collaborative design
  • separation system
  • optimal trajectory
  • State control
  • Positioning System
  • Propulsion System
  • Deep Learning
  • Sun simulator
  • Sloshing
  • redundancy
  • Bipropellant propulsion system
  • Primary breakup
  • Space weather
  • Thrust
  • Asteroid Apophis
  • Launch abort system
  • STK software
  • Flexible satellite
  • Position determination
  • Pulse-Width Pulse-Frequency Modulator
  • Shooting Method
  • Adaptive attitude control
  • Reconfiguration
  • Space industry
  • HZETRN
  • Optimized environment
  • Cold gas thruster
  • Attitude determination and control subsystem
  • breast cancer
  • linear Instability
  • Turbulent Flow
  • Control Allocation
  • LEO Orbit
  • Nonlinear Quadratic Tracking (NQT)
  • Integrated Navigation
  • space structures
  • CanSat
  • PSO optimization
  • Magnetic field
  • sensitivity matrix
  • Hardware in the loop
  • Differential flatness
  • Hydrazine