Journal of Aerospace Science and Technology

Journal of Aerospace Science and Technology

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i10-index 51
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Number of Volumes 19
Number of Issues 45
Number of Articles 357
Number of Contributors 601
Article View 315,820
PDF Download 169,637
View Per Article 884.65
PDF Download Per Article 475.17
 
Accepted Submissions 388
Acceptance Rate 58
Time to Accept (Days) 212
Number of Indexing Databases 9
Number of Reviewers 633

 

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

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