Journal of Aerospace Science and Technology

Journal of Aerospace Science and Technology

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Number of Volumes 19
Number of Issues 45
Number of Articles 350
Number of Contributors 591
Article View 302,721
PDF Download 154,266
View Per Article 864.92
PDF Download Per Article 440.76
 
Accepted Submissions 386
Acceptance Rate 58
Time to Accept (Days) 212
Number of Indexing Databases 9
Number of Reviewers 621

 

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
  • Finite Element
  • Genetic Algorithm
  • numerical simulation
  • Kalman Filter
  • Quadrotor
  • Helicopter
  • Extended Kalman Filter
  • Cylindrical Shell
  • Optimal guidance
  • Lyapunov Stability
  • Flight Dynamics
  • Integrated guidance and control
  • GPS
  • Deep Learning
  • Finite element method
  • Particle Swarm Optimization (PSO)
  • Two-phase flow
  • heat transfer
  • Fuzzy logic
  • aerodynamic coefficients
  • guidance
  • Simulation
  • Buckling
  • Flight simulation
  • Nonlinear
  • Direct Collocation
  • Trajectory Tracking
  • Mathematical Modeling
  • Vortex-induced vibration
  • Adaptive control
  • Compressor
  • Aerodynamic
  • Winglet
  • constrained optimization
  • Piezoelectric
  • Aircraft
  • Design of Experiment (DoE)
  • Dynamic Modeling
  • PSO algorithm
  • Post-buckling
  • CubeSat
  • Epoxy
  • Dielectric Barrier Discharge
  • the characteristic curve
  • Porous material
  • Attitude control
  • Large Eddy Simulation
  • launcher
  • Sliding mode control
  • Iran
  • Robust predictive control
  • Computational Fluid Dynamics
  • EKF
  • Aluminum matrix composite
  • Spacecraft attitude control
  • Boundary element method (BEM)
  • Subsonic
  • Transition Flight
  • attitude estimation
  • Central composite design
  • Radiation
  • Flow Separation
  • Integrated Navigation
  • Reliability
  • Preload
  • Strouhal number
  • Seeker Noise
  • “System Identification”
  • Neural Network
  • Bluff Body
  • Dynamic Response
  • Miss Distance Analysis
  • Combustion chamber
  • Centrifugal pump
  • UAV
  • B-spline curves
  • Pressure distribution
  • rotor
  • maneuverability
  • Porous media
  • Thermal buckling
  • Robust Control
  • Experimental Aerodynamics
  • Multidisciplinary design optimization
  • PID Controller
  • Gear train
  • Flutter
  • Trajectory Optimization
  • Error compensation
  • Unmanned aerial vehicles
  • Three-body problem
  • Optimization layout gears
  • Droplet
  • plasma actuator
  • Parameter optimization
  • Flow control
  • Morphing wing
  • Aeroelasticity
  • Dynamic Inversion
  • Quadrotor UAV
  • 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
  • Damped natural frequencies
  • Parts configuration
  • 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
  • De-orbiting
  • Turbulence model
  • CFD video technique
  • Optimum parameters
  • Gurney flap
  • Lattice Boltzmann equation
  • hybrid wick
  • Type2 fuzzy logic
  • Formation flight
  • Modified Predictive Kalman Filter (MPKF)
  • Asteroid
  • Inverse simulation
  • Feedback linearization
  • Polymer nanocomposite
  • Clear air turbulence
  • Aerodynamic configuration
  • second order sliding mode control
  • Flow interference
  • stiffness effects
  • Self Alignment
  • Adaptive Mutation
  • atomization
  • Derived Gas Turbine
  • SST K-??turbulence model
  • 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
  • Galloping
  • cold flow simulation
  • Fiber Matrix Debonding
  • Feedback-linearization
  • Rotor overlap sweep
  • Sensitivity analysis
  • Vibration Analysis
  • winding pattern

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