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
  • Remote Sensing
  • system design
  • Microgravity
  • numerical simulation
  • Satellite attitude control
  • Optimal control
  • Kalman Filter
  • Spacecraft
  • Launch Vehicle
  • Simulation
  • GPS
  • Multidisciplinary design optimization
  • Swirl injector
  • Sounding rocket
  • Reliability
  • Optimal guidance
  • Reaction wheels
  • Pitch program
  • Guidance law
  • CubeSat
  • Air bearing
  • Thruster
  • Monopropellant thruster
  • Satellite Constellations
  • Extended Kalman Filter
  • Attitude determination
  • Nozzle
  • guidance
  • Sensitivity analysis
  • remote sensing satellite
  • LEO satellite
  • attitude estimation
  • Low thrust
  • Liquid Propellant Engine
  • Finite Element
  • heat transfer
  • flexible spacecraft
  • Saturation
  • INS
  • star sensor
  • Helmholtz coil
  • Star tracker
  • TLE
  • Inertial Navigation System
  • Outer space
  • fault detection
  • 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
  • Reentry
  • Hypersonic Flow
  • Star catalog
  • Space Capsule
  • Neural Network
  • Spray cone
  • Modeling
  • 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
  • design requirements
  • Numerical modeling
  • injection
  • Artificial Neural Network
  • design algorithm
  • Responsibility
  • decomposition chamber
  • orbital mechanics
  • IMU
  • Sandwich panels
  • Capillary injector
  • EKF
  • Orbit Determination
  • Starlink
  • 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
  • Antenna Pointing Mechanism
  • Reconfiguration
  • 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
  • Adaptive attitude control
  • Communication satellite
  • Space industry
  • Pulse-Width Pulse-Frequency Modulator
  • HZETRN
  • Control Allocation
  • space launch vehicle
  • breast cancer
  • linear Instability
  • Turbulent Flow
  • Attitude determination and control subsystem
  • LEO Orbit
  • Nonlinear Quadratic Tracking (NQT)
  • space structures
  • Optimized environment
  • CanSat
  • Integrated Navigation
  • Magnetic field
  • sensitivity matrix
  • Hardware in the loop
  • Differential flatness
  • PSO optimization