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


          

 

Current Issue: Volume 18, Issue 4, 2025 

Evaluating Optimal Ultrasound to Deform the Blood Clot in a Vessel for Astronauts Health

Pages 22-31

10.22034/jsst.2025.1519

Ramin Kamalimoghadam, Mahmoud Najafi, Masoomeh Azadegan, Nasrin Sahranavardfar

Keywords Cloud

  • Attitude control
  • satellite
  • Genetic Algorithm
  • optimization
  • Uncertainty
  • Reaction wheel
  • Space Radiation
  • Conceptual design
  • system design
  • Microgravity
  • Remote Sensing
  • numerical simulation
  • Satellite attitude control
  • Simulation
  • Launch Vehicle
  • Kalman Filter
  • Spacecraft
  • Optimal control
  • GPS
  • Multidisciplinary design optimization
  • Swirl injector
  • Sounding rocket
  • Optimal guidance
  • Reliability
  • Thruster
  • Reaction wheels
  • Pitch program
  • Guidance law
  • CubeSat
  • Extended Kalman Filter
  • Monopropellant thruster
  • Air bearing
  • Satellite Constellations
  • Attitude determination
  • Nozzle
  • guidance
  • Sensitivity analysis
  • Liquid Propellant Engine
  • remote sensing satellite
  • Star tracker
  • LEO satellite
  • attitude estimation
  • Low thrust
  • Finite Element
  • TLE
  • Saturation
  • INS
  • star sensor
  • Helmholtz coil
  • flexible spacecraft
  • 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
  • Inertial Navigation
  • Modeling
  • Star catalog
  • Reentry
  • Hypersonic Flow
  • Neural Network
  • Spray cone
  • Space Capsule
  • Ground station
  • Displacement damage
  • Radiation
  • GEO satellite
  • Numerical analysis
  • Solar Cell
  • Fuzzy logic
  • Electrical power subsystem
  • spacecraft formation flying
  • Calibration
  • Magnetometer
  • vibration
  • Machine Learning
  • Robust Control
  • Composite
  • Sliding mode
  • launcher
  • LQR
  • Design optimization
  • Hydrogen peroxide
  • Catalyst
  • Microsatellite
  • Space
  • Terminal sliding mode
  • 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
  • Orbit Determination
  • Starlink
  • Radiation damage
  • Fault Isolation
  • Combustion chamber
  • heat flux
  • growth
  • Orbital maneuver
  • 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
  • Bipropellant propulsion system
  • Collaborative design
  • separation system
  • State control
  • Propulsion System
  • Positioning System
  • Deep Learning
  • Sun simulator
  • Sloshing
  • redundancy
  • Primary breakup
  • Space weather
  • Asteroid Apophis
  • Thrust
  • optimal trajectory
  • Launch abort system
  • STK software
  • Space Traffic Management
  • Position determination
  • Flexible satellite
  • Shooting Method
  • Pulse-Width Pulse-Frequency Modulator
  • Reconfiguration
  • Adaptive attitude control
  • Space industry
  • HZETRN
  • Optimized environment
  • space launch vehicle
  • breast cancer
  • linear Instability
  • Turbulent Flow
  • Control Allocation
  • 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