Journal of Technology in Aerospace Engineering

Journal of Technology in Aerospace Engineering

Number of Volumes 10
Number of Issues 39
Number of Articles 243
Number of Contributors 435
Article View 441942
PDF Download 164,760
View Per Article 1818.69
PDF Download Per Article 678.02
 
Number of Submissions 479
Acceptance Rate 45
Time to Accept (Days) 185
Number of Indexing Databases 0
Number of Reviewers 557

Journal of Technology in Aerospace Engineering (JTAE), is an open access double blind peer reviewed quarterly publication which publishes high quality papers on all aspects of Air and Space engineering include: Technology in guidance, control and navigation, Technology in structure and aerospace mechanisms, Technology in aerospace vehicles design, Technology in aerospace applications, Technology in aerospace bio-medicine, Technology in Propulsion systems, Technology in materials and their applications in aerospace engineering. The Journal of Technology in Aerospace Engineering (JTAE) owned, managed and published by Aerospace Research Institute has been publishing papers in Farsi (Abstracts in English) since September 2017.

Currently, the journal systematically publishes 24 articles annually, distributed across four issues in Persian (with English abstracts), thereby providing a worthy platform for showcasing the scientific achievements of researchers in the country to interested readers.


Publication Fee: Article processing charges and any other publication fees in the Journal of Technology in Aerospace Engineering are free for authors.
Subscription Fee: Journal of Technology in Aerospace Engineering Publishes as an open-access electronic journal, so audiences have no subscription fee. 

Bibliography Method: IEEE , EndNote 


The Journal of Technology in Aerospace Engineering (JTAE) also follows the Committee on Publication Ethics (COPE) Regulations. 

All submitted manuscripts are checked for similarity through a trustworthy software named Hamanandjo software to be assured about its originality and then rigorously peer-reviewed by the international reviewers.


All articles are published under the terms of the Creative Commons Attribution License (CC BY)


Having an ORCID identifier is mandatory for all authors. You can register at https://orcid.org/register.


   


 

Current Issue: Volume 10, Issue 3, Autumn 2026 

Keywords Cloud

  • Microgravity
  • Computational Fluid Dynamics
  • numerical simulation
  • UAV
  • satellite
  • optimization
  • Neural Network
  • Combustion chamber
  • Spacecraft
  • heat transfer
  • Conceptual design
  • plants
  • Integrated guidance and control
  • Statistical design
  • Unmanned Aerial Vehicle
  • Q-Learning
  • Turbofan Engine
  • burning rate
  • Genetic Algorithm
  • Helicopter
  • Remote Sensing
  • aerodynamic coefficients
  • missile
  • Reliability
  • Life support system
  • Dynamic Modeling
  • CubeSat
  • Adaptive control
  • Radiation
  • Sliding Mode Controller
  • Combustion efficiency
  • Flying Robot
  • Modal Analysis
  • Exergy
  • DNA damage
  • Space debris
  • Particle Swarm Optimization
  • Stability
  • Composite
  • Electric Propulsion
  • rarefied Gas Flow
  • Formation flight
  • Astrobiology
  • Flat plate
  • Monopropellant thruster
  • Model predictive Control
  • Fault Tolerant Control
  • Flexible Structures
  • Aviation industry
  • Multidisciplinary design optimization
  • Technology Development
  • Turbulence model
  • Attitude control
  • Reinforcement Learning
  • Finite element method
  • Re-entry
  • Fuzzy logic
  • Aerodynamics
  • Clinostat
  • Modeling
  • Gravity
  • Ramjet
  • experimental study
  • Phenolic Compounds
  • Flutter
  • Robust sliding mode control
  • sandwich structure
  • turbojet engine
  • Dissipative Particle Dynamics
  • Finite strip Method
  • Follower aircraft
  • vibration control
  • Modified Rodrigues parameters
  • CFD
  • Drone
  • Hypersonic Flow
  • Scramjet
  • Two-Dimensional Numerical Analysis
  • Flight safety
  • flexible spacecraft
  • Space travel
  • Antioxidant enzymes
  • Nonlinear Control
  • Honeycomb
  • aerodynamic optimization
  • Air Taxi
  • Space explorations
  • Direct Simulation Monte Carlo
  • Noise
  • Plant
  • Optimal control
  • the Second Law of Thermodynamics
  • Aeroelasticity
  • PBN
  • Solid fuel propellants
  • Weight
  • Horizontal Tail
  • Defense
  • Socioeconomic impacts
  • Trust
  • Search and rescue
  • Space missions
  • Catalytic Bed Porosity
  • flapping flight
  • parametric uncertainty
  • Roughness
  • Taguchi algorithm
  • Morphing Wings
  • Reflected Shock Tube
  • Shear Thinning
  • gray wolf optimization algorithm
  • fatigue behavior high cycle
  • Origin life
  • Mechatronics Engineering
  • Fault diagnosis and prognostics
  • Thermal Load
  • selective laser melting
  • Can bus protocol
  • Micro-airfoil
  • Separation bubble
  • Unmanned mission
  • Erosive Burning
  • Energy Absorption Capacity
  • Solid propellant
  • Sunshield
  • Turbulence
  • Bonding Agent
  • UAV Control
  • RNAV
  • Economic model
  • Curiosity
  • Nonlinear dynamic absorber
  • Endless runway
  • Ground vibrations
  • VTOL Aircraft
  • A* Algorithm
  • De-orbiting
  • photosynthesis
  • Automatic Control System
  • lily
  • topic modeling
  • PID Controller
  • Solar Radiation
  • Civil Drone
  • Markov Modeling
  • atomization
  • Control surfaces
  • Cylindrical Waveguide Technology
  • decision tree
  • processor-in-the-loop Implementation
  • Landsat 8
  • Wavy airfoil
  • Carbon Nanotube
  • Active method
  • plates
  • Mutual inductance
  • Inverse dynamic controller
  • \"
  • Wing
  • Thrust Control Vector (TVC)
  • Aerodynamic
  • Renewable Energy
  • Laminated composite
  • Regression approaches
  • Can bus analyzer
  • Solare Flare
  • Load Factor
  • Bird-like
  • formation control
  • Converging-Diverging Nozzle
  • UGF
  • Flow Visualization
  • Tectonic stress
  • LBM
  • Experimental analysis
  • Asteroid Mining
  • Natural frequency.Damping factor
  • manned spacecraft
  • solar panels
  • Adaptive control-target
  • کنترل جریان
  • piezoelectric patches
  • Pitch Compensator
  • flight control
  • Swirl injector
  • SSPA
  • Asymmetrical Bandpass Filter
  • Wing Fence
  • Submerged nozzle
  • Six-Degree-of-Freedom Simulation
  • meshless numerical method
  • Airport charges
  • Iran aerial market profile
  • Boundary Layer
  • position and attitude coupling
  • Space Propulsion
  • Damage
  • Internal Flow
  • Miniaturization
  • growth

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