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 301,572
PDF Download 152,669
View Per Article 861.63
PDF Download Per Article 436.2
 
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
  • Finite Element
  • Genetic Algorithm
  • Kalman Filter
  • numerical simulation
  • Helicopter
  • Quadrotor
  • Extended Kalman Filter
  • Cylindrical Shell
  • Flight Dynamics
  • Fuzzy logic
  • Lyapunov Stability
  • Integrated guidance and control
  • Two-phase flow
  • Deep Learning
  • Particle Swarm Optimization (PSO)
  • Simulation
  • Optimal guidance
  • GPS
  • guidance
  • aerodynamic coefficients
  • heat transfer
  • Finite element method
  • Buckling
  • Flight simulation
  • Nonlinear
  • Direct Collocation
  • Trajectory Tracking
  • Mathematical Modeling
  • 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
  • delta wing
  • Iran
  • the characteristic curve
  • EKF
  • Aluminum matrix composite
  • Spacecraft attitude control
  • Robust predictive control
  • B-spline curves
  • Computational Fluid Dynamics
  • attitude estimation
  • Boundary element method (BEM)
  • Subsonic
  • Central composite design
  • Large Eddy Simulation
  • Flow Separation
  • Integrated Navigation
  • Strouhal number
  • Reliability
  • Preload
  • Uncertainty
  • Bluff Body
  • Dynamic Response
  • Miss Distance Analysis
  • Radiation
  • Centrifugal pump
  • UAV
  • Seeker Noise
  • Pressure distribution
  • “System Identification”
  • maneuverability
  • Porous material
  • Thermal buckling
  • Robust Control
  • Dielectric Barrier Discharge
  • Multidisciplinary design optimization
  • PID Controller
  • Gear train
  • rotor
  • Flutter
  • Trajectory Optimization
  • Error compensation
  • Epoxy
  • Unmanned aerial vehicles
  • Optimization layout gears
  • Droplet
  • plasma actuator
  • Parameter optimization
  • Flow control
  • Dynamic Inversion
  • Aerodynamic
  • Morphing wing
  • Quadrotor UAV
  • Composites
  • Weight/volume optimization
  • Semi-elliptical crack
  • Neural Network
  • Non-gray gas
  • Bezier Curve
  • Lift
  • Shell and tube heat exchanger
  • Solar Sail Assembly
  • Ducted Fan
  • CNT
  • surge
  • Damped natural frequencies
  • Parts configuration
  • Gas Generator
  • Booster Landing
  • Interaction Force
  • Air Accident
  • shock interactions
  • Ballistic
  • point loads
  • Turbulence
  • Force Measurement
  • Gimballed IMU
  • Boltzmann equation
  • Drag and lift coefficient
  • Dynamic analysis
  • Matrix Crack
  • Springback
  • Particle Swarm Optimization
  • flutter index
  • Coupling of Attitude and Orbital Dynamics
  • Delamination
  • Vacuum Chamber
  • ............................
  • tandem spheres
  • chemical kinetics
  • Visual measurement method
  • “spacecraft”
  • Multiaxial fatigue
  • 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
  • Sensitivity analysis
  • Vibration Analysis
  • composite plates

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