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
  • Conceptual design
  • Uncertainty
  • Space Radiation
  • system design
  • Remote Sensing
  • Microgravity
  • Satellite attitude control
  • numerical simulation
  • Simulation
  • Launch Vehicle
  • Kalman Filter
  • Spacecraft
  • Optimal control
  • Multidisciplinary design optimization
  • GPS
  • Swirl injector
  • Sounding rocket
  • Optimal guidance
  • Reliability
  • Thruster
  • Reaction wheels
  • Pitch program
  • Guidance law
  • CubeSat
  • Satellite Constellations
  • Extended Kalman Filter
  • Air bearing
  • Monopropellant thruster
  • Attitude determination
  • Nozzle
  • remote sensing satellite
  • Sensitivity analysis
  • Liquid Propellant Engine
  • guidance
  • 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
  • Reentry
  • Hypersonic Flow
  • Star catalog
  • Space Capsule
  • Neural Network
  • Spray cone
  • Ground station
  • Displacement damage
  • Radiation
  • GEO satellite
  • Inertial Navigation
  • Numerical analysis
  • Solar Cell
  • Fuzzy logic
  • 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
  • Radiation damage
  • Capillary injector
  • growth
  • Orbit Determination
  • simulator
  • heat flux
  • Space law
  • Combustion chamber
  • 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
  • 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
  • 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
  • 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