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
  • Conceptual design
  • Space Radiation
  • Uncertainty
  • Reaction wheel
  • Satellite attitude control
  • Microgravity
  • system design
  • Remote Sensing
  • numerical simulation
  • Simulation
  • Kalman Filter
  • Launch Vehicle
  • Spacecraft
  • Optimal control
  • GPS
  • Multidisciplinary design optimization
  • Swirl injector
  • Optimal guidance
  • Sounding rocket
  • Reliability
  • Thruster
  • Reaction wheels
  • Pitch program
  • Guidance law
  • CubeSat
  • Extended Kalman Filter
  • Satellite Constellations
  • 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
  • heat transfer
  • TLE
  • Saturation
  • INS
  • star sensor
  • Helmholtz coil
  • flexible spacecraft
  • Outer space
  • fault detection
  • Inertial Navigation System
  • Stability Analysis
  • Sliding mode control
  • Proportional navigation
  • Geostationary orbit
  • Sovereignty
  • atomization
  • Aerodynamic heating
  • manned spacecraft
  • Microstructure
  • Transverse flow
  • image processing
  • 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
  • Electrical power subsystem
  • Solar Cell
  • Fuzzy logic
  • time series
  • Calibration
  • Magnetometer
  • vibration
  • Machine Learning
  • spacecraft formation flying
  • 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
  • Radiation damage
  • Starlink
  • 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
  • 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
  • Attitude determination and control subsystem
  • breast cancer
  • linear Instability
  • Turbulent Flow
  • Control Allocation
  • LEO Orbit
  • Nonlinear Quadratic Tracking (NQT)
  • Integrated Navigation
  • space structures
  • CanSat
  • PSO optimization
  • Magnetic field
  • sensitivity matrix
  • Hardware in the loop
  • Differential flatness
  • Hydrazine