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

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