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
  • Reaction wheel
  • Space Radiation
  • Satellite attitude control
  • Microgravity
  • Remote Sensing
  • numerical simulation
  • system design
  • Optimal control
  • Kalman Filter
  • Launch Vehicle
  • Simulation
  • Spacecraft
  • GPS
  • Multidisciplinary design optimization
  • Reliability
  • Optimal guidance
  • Swirl injector
  • Sounding rocket
  • Reaction wheels
  • Attitude determination
  • Pitch program
  • CubeSat
  • Satellite Constellations
  • Air bearing
  • Thruster
  • Nozzle
  • Monopropellant thruster
  • Guidance law
  • Extended Kalman Filter
  • guidance
  • Sensitivity analysis
  • remote sensing satellite
  • LEO satellite
  • fault detection
  • Low thrust
  • Liquid Propellant Engine
  • Finite Element
  • TLE
  • Saturation
  • star sensor
  • INS
  • Helmholtz coil
  • flexible spacecraft
  • Star tracker
  • Inertial Navigation System
  • Outer space
  • heat transfer
  • Stability Analysis
  • attitude estimation
  • Sliding mode control
  • Proportional navigation
  • Geostationary orbit
  • Sovereignty
  • atomization
  • Aerodynamic heating
  • manned spacecraft
  • Microstructure
  • Transverse flow
  • time series
  • State dependent riccati equation
  • GEO satellite
  • Neural Network
  • Star catalog
  • Reentry
  • Spray cone
  • Solar Cell
  • Fuzzy logic
  • Modeling
  • Ground station
  • Displacement damage
  • Radiation
  • Inertial Navigation
  • Numerical analysis
  • Electrical power subsystem
  • Space Capsule
  • Hypersonic Flow
  • spacecraft formation flying
  • Calibration
  • Magnetometer
  • vibration
  • Machine Learning
  • Robust Control
  • Composite
  • Sliding mode
  • Terminal sliding mode
  • launcher
  • LQR
  • image processing
  • Space
  • Hydrogen peroxide
  • Design optimization
  • Microsatellite
  • Catalyst
  • Artificial Neural Networks
  • cryogenic
  • Orbital maneuver
  • design requirements
  • Numerical modeling
  • injection
  • Artificial Neural Network
  • design algorithm
  • Responsibility
  • decomposition chamber
  • orbital mechanics
  • IMU
  • Sandwich panels
  • Starlink
  • 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
  • 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
  • Reconfiguration
  • Space industry
  • Pulse-Width Pulse-Frequency Modulator
  • 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