Journal of Aerospace Science and Technology

Journal of Aerospace Science and Technology

h-index 15
i10-index 51
google scholar

 

Number of Volumes 19
Number of Issues 45
Number of Articles 350
Number of Contributors 591
Article View 301,648
PDF Download 152,805
View Per Article 861.85
PDF Download Per Article 436.59
 
Accepted Submissions 385
Acceptance Rate 58
Time to Accept (Days) 211
Number of Indexing Databases 9
Number of Reviewers 615

 

I am pleased to introduce this new journal in aerospace science and technology. Journal of Aerospace Science and Technology is an open-access, double-blind, peer-reviewed semiannual publication published by the Iranian Aerospace Society. As we understand, there is little or no forum in this field with an international scope in the region of central and west Asia. Therefore we strongly believe that it will make it possible in the region and in the whole world for better communication among scientists and researchers in aeronautical and astronautical sciences and technologies, and also in all related fields as aerodynamics and fluid mechanics, thermodynamics, and propulsion, combustion and heat transfer, dynamics and control, flight mechanics, design, structures and vibration, aviation management, etc.  To start a new submission, please first read the Guide for Authors page for detailed information about manuscript format, style, and other requirements. Manuscript submission, refereeing, and publishing are completely free of charge. New manuscripts should be submitted online by the corresponding author through the website after registration. This journal follows the Committee on Publication Ethics (COPE) and complies with the highest ethical standards following ethical laws. (Read more about this journal...)


It is necessary for authors to register a unique ORCID research ID in this publication. 
It is necessary to enter the exact details of the department, faculty, university, province, country, and ORCID research ID in the authors' affiliation section when registering the article.

Please note that the new email address for the  journal is as follows:
 jastanjoman@gmail.com
Publication order: Semiannual
Language: English
Rank in the Ministry of Science of IRAN: A
Type publication: Online
Type of Access: Open access (full text)

All articles published in the journal are in a state of open access for the public to study or scientific exploit following the principles of research and correct citation.

 

Current Issue: Volume 18, Issue 2, 2025 

Quasi-static and Dynamic Analysis of a 12U Cubesat Under Flight-phase Environmental Loads

Pages 88-98

10.22034/jast.2025.475926.1207

Amirreza Haddadi, Seyed mohammad navid Ghoreishi, Yaser Sedigh, Hossein Shabani

Keywords Cloud

  • optimization
  • CFD
  • Wind tunnel
  • Genetic Algorithm
  • Finite Element
  • numerical simulation
  • Kalman Filter
  • Quadrotor
  • Helicopter
  • Extended Kalman Filter
  • Optimal guidance
  • Fuzzy logic
  • Flight Dynamics
  • Lyapunov Stability
  • Integrated guidance and control
  • Two-phase flow
  • Deep Learning
  • Particle Swarm Optimization (PSO)
  • Cylindrical Shell
  • heat transfer
  • aerodynamic coefficients
  • guidance
  • GPS
  • Simulation
  • Finite element method
  • Buckling
  • Flight simulation
  • Nonlinear
  • Direct Collocation
  • Trajectory Tracking
  • Dynamic Inversion
  • Vortex-induced vibration
  • Adaptive control
  • Compressor
  • Attitude control
  • constrained optimization
  • Porous media
  • Piezoelectric
  • Aircraft
  • Design of Experiment (DoE)
  • Dynamic Modeling
  • PSO algorithm
  • Post-buckling
  • CubeSat
  • Transition Flight
  • Three-body problem
  • Experimental Aerodynamics
  • Winglet
  • launcher
  • Aeroelasticity
  • Combustion chamber
  • Sliding mode control
  • Iran
  • the characteristic curve
  • Robust predictive control
  • EKF
  • Aluminum matrix composite
  • Spacecraft attitude control
  • B-spline curves
  • Computational Fluid Dynamics
  • Boundary element method (BEM)
  • attitude estimation
  • Subsonic
  • Central composite design
  • Large Eddy Simulation
  • Flow Separation
  • Integrated Navigation
  • Neural Network
  • Reliability
  • Preload
  • Strouhal number
  • Seeker Noise
  • Bluff Body
  • Dynamic Response
  • Miss Distance Analysis
  • Radiation
  • Centrifugal pump
  • UAV
  • “System Identification”
  • Pressure distribution
  • rotor
  • maneuverability
  • Porous material
  • Thermal buckling
  • Robust Control
  • Dielectric Barrier Discharge
  • Multidisciplinary design optimization
  • PID Controller
  • Gear train
  • Flutter
  • Trajectory Optimization
  • Error compensation
  • Unmanned aerial vehicles
  • Epoxy
  • Optimization layout gears
  • Droplet
  • plasma actuator
  • Parameter optimization
  • Flow control
  • Quadrotor UAV
  • Morphing wing
  • Aerodynamic
  • Mathematical Modeling
  • Weight/volume optimization
  • Composites
  • Semi-elliptical crack
  • delta wing
  • Uncertainty
  • Non-gray gas
  • Bezier Curve
  • Lift
  • Solar Sail Assembly
  • Shell and tube heat exchanger
  • Ducted Fan
  • CNT
  • surge
  • Parts configuration
  • Damped natural frequencies
  • Gas Generator
  • Booster Landing
  • Interaction Force
  • Air Accident
  • shock interactions
  • Ballistic
  • point loads
  • Turbulence
  • Drag and lift coefficient
  • Matrix Crack
  • Boltzmann equation
  • Force Measurement
  • Dynamic analysis
  • Gimballed IMU
  • Springback
  • Particle Swarm Optimization
  • flutter index
  • Coupling of Attitude and Orbital Dynamics
  • Delamination
  • Vacuum Chamber
  • ............................
  • tandem spheres
  • Multiaxial fatigue
  • Visual measurement method
  • “spacecraft”
  • chemical kinetics
  • GPS Spoofing
  • “Self-tuning Regulators”
  • gray wolf optimization algorithm
  • Transonic
  • axial-flow compressor
  • Magnetometer calibration
  • the critical cavitation number
  • robustness
  • Airplane wing
  • CFD video technique
  • Turbulence model
  • De-orbiting
  • Optimum parameters
  • Gurney flap
  • Modified Predictive Kalman Filter (MPKF)
  • hybrid wick
  • Type2 fuzzy logic
  • Formation flight
  • Lattice Boltzmann equation
  • Asteroid
  • Inverse simulation
  • Feedback linearization
  • Polymer nanocomposite
  • Clear air turbulence
  • Aerodynamic configuration
  • second order sliding mode control
  • Flow interference
  • atomization
  • Self Alignment
  • Adaptive Mutation
  • stiffness effects
  • SST K-??turbulence model
  • Derived Gas Turbine
  • Hingeless
  • Shape Optimization
  • apparent mass
  • High Aspect Ratio Wings
  • Pilot-Induced Oscillation
  • Actuator Fault
  • robust flight control
  • Multi-Input - Multi-Output Controller
  • Orbit Determination
  • Robot- Flexible Link- Finite Element- Maximum Allowable Dynamic Load
  • Boundary Layer
  • Premixed Flames
  • discrete element method
  • GENEX guidance
  • Cantilever cylindrical thick shell
  • high speed and high altitude target
  • cold flow simulation
  • Fiber Matrix Debonding
  • Feedback-linearization
  • Rotor overlap sweep
  • Vibration Analysis
  • Sensitivity analysis
  • composite plates

Related Journals