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