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
  • Conceptual design
  • Space Radiation
  • Reaction wheel
  • system design
  • numerical simulation
  • Remote Sensing
  • Microgravity
  • Satellite attitude control
  • Optimal control
  • Spacecraft
  • Kalman Filter
  • Simulation
  • Launch Vehicle
  • GPS
  • Multidisciplinary design optimization
  • Reliability
  • Sounding rocket
  • Swirl injector
  • Optimal guidance
  • Reaction wheels
  • Attitude determination
  • Pitch program
  • CubeSat
  • Monopropellant thruster
  • Nozzle
  • Thruster
  • Air bearing
  • Satellite Constellations
  • Extended Kalman Filter
  • Guidance law
  • remote sensing satellite
  • Sensitivity analysis
  • guidance
  • LEO satellite
  • fault detection
  • Low thrust
  • Liquid Propellant Engine
  • Finite Element
  • heat transfer
  • TLE
  • Saturation
  • star sensor
  • flexible spacecraft
  • INS
  • Star tracker
  • Helmholtz coil
  • Outer space
  • Stability Analysis
  • attitude estimation
  • Sliding mode control
  • Inertial Navigation System
  • Proportional navigation
  • Geostationary orbit
  • Sovereignty
  • atomization
  • Aerodynamic heating
  • manned spacecraft
  • Microstructure
  • Transverse flow
  • vibration
  • State dependent riccati equation
  • Neural Network
  • Star catalog
  • Reentry
  • Spray cone
  • Solar Cell
  • Fuzzy logic
  • Ground station
  • Displacement damage
  • Radiation
  • Inertial Navigation
  • GEO satellite
  • Modeling
  • Calibration
  • time series
  • Space Capsule
  • Hypersonic Flow
  • Magnetometer
  • Machine Learning
  • spacecraft formation flying
  • Numerical analysis
  • 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
  • design requirements
  • Numerical modeling
  • injection
  • Artificial Neural Network
  • design algorithm
  • Responsibility
  • decomposition chamber
  • orbital mechanics
  • IMU
  • Sandwich panels
  • Starlink
  • EKF
  • Radiation damage
  • Capillary injector
  • 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
  • Nonlinear Quadratic Tracking (NQT)
  • LEO Orbit
  • Differential flatness
  • Optimized environment
  • space structures
  • CanSat
  • Attitude determination and control subsystem
  • Magnetic field
  • Hardware in the loop
  • sensitivity matrix
  • Integrated Navigation
  • Hydrazine