Aerospace Mechanics

Aerospace Mechanics

Journal Information


According to the latest review and ranking of the country's scientific Journals in the Islamic World Science Citation Database (ISC), the scientific Journal of Aerospace Mechanics has been ranked Q3 in terms of quality.

This Journal , which is published by the technical and engineering faculty and research institute of Imam Hossein University (AS), under license 3/2910/472 dated 5/26/ 83 of the Ministry of Science, Research and Technology under the title "Aerospace Mechanics" has been published with a scientific-research degree.

This Journal publish the latest achievements of the country's researchers, which are the result of original research and contain new results in the specialized fields of the following five main trends:

  1. Vibration dynamics and control
  2. Solid Mechanics
  3. Propulsion and heat transfer
  4. Manufacturing and Production
  5. Impact mechanics

  • Type of Access: Open Access (OA) 
  • Start of Journal : 2005
  • Credit of the Journal : Scientific-Research
  • Type of articles to be published: Research
  • Format: Print and Online
  • Frequency: Quarterly
  • Language: Persian; including English abstracts
  • Coverage: Theories, Models and Systems Related of Aerospace Mechanics
  • Type of peer-review: Double Blind Peer Review; two reviewers
  • Initial review period: 1 week
  • Average time for review articles: Maximum 20 days
  • Manual of style of the Journal : Vancouver
  • Article Processing, Publishing and judging Charges: Free for review process and Journal
  • Contact E-mail: Havafaza@ihu.ac.ir
  • Cooperation with the association: Scientific Association of High Energy Materials of Iran
  • Type of License: CC BY-NC

Audience: The audience of this Journal is made up of professors, academic faculty members of universities, experts in mechanics and related fields.

Faculty members, researchers, and graduate students are invited to prepare their Persian article according to the article preparation guide and by visiting the Journal website (http://maj.ihu.ac.ir) and registering in it, Send the electronic version of the article to the Journal office.

** Submitted articles must not have been previously published in any Journal .**

  1. Respected authors are requested to follow the format of the Journal in order to speed up the review and judging process.
  2. Respecting the rules of ethics in Journals, this Journal  is subject to the rules of the Committee on Ethics in Journals  (COPE) and follows the executive regulations of the Law on Prevention and combating fraud in Scientific Works.
  3. All articles sent to this  Journal  are reviewed by plagiarism software. Submitting the report of Samim Noor similarity  check system or Irandak similarity  check system is also necessary at the time of submitting the article. (Link to the guide to the plagiarism detector system)
  4. Also, please, when submitting the article (commitment form), (authors conflict of interest form) and form (authors' Profile) must be signed by all authors and uploaded to the system.
Current Issue: Volume 22, Issue 2 - Serial Number 84, Summer 2026 

Investigating Dynamics of the Cubesat Inside the P-Pod Considering Affecting Parameters

Pages 13-24

10.47176/MAJ.2026.1557

Arezoo Esmaeili, Moharram Shameli, Seyed Tohid Khandani Kuzehkonan, Gholamreza Hashemi

Keywords Cloud

  • Numerical Simulation
  • Sliding Mode Control
  • genetic algorithm
  • Natural frequency
  • Buckling
  • Optimization
  • Heat Transfer
  • Composite
  • Mechanical Properties
  • Finite Element
  • Carbon nanotube
  • Cylindrical Shell
  • Inertial Navigation
  • Robust Control
  • Kalman Filter
  • Functionally graded material
  • Piezoelectric
  • Energy Absorption
  • Response Surface Methodology
  • Energy harvesting
  • Extended State Observer
  • Additive manufacturing
  • First order shear deformation theory
  • Stability
  • Gyroscope
  • Repeated loading
  • Active vibration control
  • Triangular plate
  • neural network
  • Guidance and Control
  • Model Predictive Control
  • differential quadrature method
  • Nonlinear vibrations
  • Multidisciplinary Design Optimization
  • Finite Element Method
  • Dynamic loading
  • Extended Kalman Filter
  • Sandwich Panel
  • free vibration
  • Force Control
  • Composite Material
  • Chattering
  • FGM
  • Sandwich panels
  • Sliding Mode
  • Elastic foundation
  • Flexible spacecraft
  • third order shear deformation theory
  • Graphene
  • Molecular Dynamics
  • Output Power
  • Shock tube
  • Frequency
  • Low velocity impact
  • Finite Element Simulation
  • Multi-Objective Optimization
  • Nanofluid
  • Fuzzy Controller
  • Multi-agent system
  • ballistic limit
  • Piezoelectric layer
  • Location of Piezoelectric
  • Hybrid nanofluids
  • Data Fusion
  • Spacecraft
  • Cylindrical shells
  • Trajectory Optimization
  • Vibration
  • Transverse Step
  • Temperature
  • Numerical study
  • Underactuated system with two degrees of freedom
  • Turbofan Engine
  • Molecular dynamics simulations
  • Fault tolerant control
  • Nonlinear Beam
  • Twisted Tape
  • Attitude control
  • Free vibrations
  • Nonlinear vibration
  • Wave Propagation
  • Tensegrity structure
  • Integrated navigation system
  • Impact
  • instability
  • Blast Loading
  • Experimental Investigation
  • Composite beam
  • finite element analysis
  • Magnetic Field
  • Mechanical Vibrations
  • Non-Newtonian nanofluid
  • Formation control
  • Fuzzy Logic
  • Stress Intensity Factor
  • Dynamic Analysis
  • Backstepping Control
  • CAD/CAM
  • Natural Convection
  • Female die
  • Grain refinement
  • Central Composite Design
  • Forced Vibration
  • Shape memory alloy
  • ANFIS
  • Rotating beam
  • Particle Filter
  • Numerical Method
  • Fracture Mechanics
  • Nonlinear model predictive control
  • Signal Processing
  • PID Controller
  • Structured and Un-structured uncertainties
  • Combustion Chamber
  • Predictive Control
  • Inertial Navigation System (INS)
  • Mixing efficiency
  • Gaseous detonation
  • Gas Turbine
  • Interfacial shear strength
  • Underwater explosion
  • Die forming
  • Uncertainty
  • Terminal Sliding Mode Control
  • Force Density
  • Image Processing
  • Severe plastic deformation
  • Turbulent Flow
  • Continuum approximation method
  • Deflection
  • Fuzzy System
  • Parameter uncertainty
  • Jump Phenomenon
  • Modal Analysis
  • Filament collection speed
  • Inertial Navigation System
  • Deep Neural Network
  • Composite lattice structures
  • Vibrations Analysis
  • Inertial Forces
  • Thrust Chamber
  • Corrosion
  • Hybrid Composite Laminate
  • DOM
  • Generalized &alpha
  • Adaptive backstepping approach
  • Flight Control System
  • Optimal Guidance
  • Radial Pressure
  • Combined actuator fault
  • Surface Mounting
  • Frequency Response
  • 3D-Printing
  • Active steering control
  • Linear Model
  • Operational Frequency
  • Dynamic Performance
  • Based Sizing Reference State of Charge Aircraft Simulation
  • Runge Kutta method
  • Nondestructive Test
  • mold temperature
  • Model uncertainty
  • Nonlinear Programming
  • Piezoelectric Layers
  • Calorimetry
  • Extruder
  • simultaneous symmetrical impulsive loading
  • Experimental study
  • Oblique blast loading
  • Film Cooling
  • Adaptive sliding mode control
  • Thick Plate
  • Dynamic Optimization
  • Porosity
  • Channel
  • Environmental test
  • critical lane change maneuver
  • Fuzzy C-Means
  • Aerodynamic Interference
  • Mode Observer Reduced
  • Volumetric radiation
  • Tube based Model Predictive Control
  • Calibration
  • Attitude Dynamics and Control
  • Emergency Condition
  • Flight Performance
  • Fuzzy approximator
  • Cooling flow field
  • Friction factor
  • Neural Controller
  • GAX cycle
  • Phase transformation models
  • Monolayer
  • Robust Guidance
  • Optimized geometry
  • Geometrical tolerances
  • Backing Material
  • Pad
  • Frictional work
  • Cold gas thrusters

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