IJRTI
International Journal for Research Trends and Innovation
International Peer Reviewed & Refereed Journals, Open Access Journal
ISSN Approved Journal No: 2456-3315 | Impact factor: 8.14 | ESTD Year: 2016
Scholarly open access journals, Peer-reviewed, and Refereed Journals, Impact factor 8.14 (Calculate by google scholar and Semantic Scholar | AI-Powered Research Tool) , Multidisciplinary, Monthly, Indexing in all major database & Metadata, Citation Generator, Digital Object Identifier(DOI)

Call For Paper

For Authors

Forms / Download

Published Issue Details

Editorial Board

Other IMP Links

Facts & Figure

Impact Factor : 8.14

Issue per Year : 12

Volume Published : 11

Issue Published : 119

Article Submitted : 23355

Article Published : 9033

Total Authors : 23952

Total Reviewer : 831

Total Countries : 162

Indexing Partner

Licence

This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License
Published Paper Details
Paper Title: Structural Analysis and Validation of a 1U CubeSat Frame Using Finite Element Analysis
Authors Name: Chinchinalli Patel Vaishnavi , Sanjita Mohanty , K Arun Kumar
Download E-Certificate: Download
Author Reg. ID:
IJRTI_211086
Published Paper Id: IJRTI2604017
Published In: Volume 11 Issue 4, April-2026
DOI:
Abstract: CubeSat satellites are used extensively to perform inexpensive space missions and technology tests due to their compact sizes. Structural integrity during launch operation, which is characterized by extreme mechanical loading, is essential to ensure successful CubeSat missions. In this work, the structural integrity of a 1U CubeSat satellite frame (100 mm × 100 mm × 100 mm) was analyzed and validated numerically using finite element method. The findings were compared to previous CubeSat studies to prove the numerical reliability. The CubeSat satellite structure was modeled in three dimensions using the software package ANSYS Mechanical, material properties of aluminum alloy were applied, and load of acceleration was imposed under the condition of fixing its base surface, simulating the deployment process. Numerical results revealed maximal displacement value of 2.474 × 10⁻⁶ m and a value of maximum von-Mises stress of 0.556 MPa, which both fall well below the material strength values. Mesh independence analysis was carried out in order to confirm the numerical stability of results.
Keywords: CubeSat, Finite Element Analysis (FEA), Structural Analysis, Nanosatellite Structures, Launch Acceleration, Aluminum Alloy, Mesh Independence Study.
Cite Article: "Structural Analysis and Validation of a 1U CubeSat Frame Using Finite Element Analysis", International Journal for Research Trends and Innovation (www.ijrti.org), ISSN:2456-3315, Vol.11, Issue 4, page no.a129-a137, April-2026, Available :http://www.ijrti.org/papers/IJRTI2604017.pdf
Downloads: 00099
ISSN: 2456-3315 | IMPACT FACTOR: 8.14 Calculated By Google Scholar| ESTD YEAR: 2016
An International Scholarly Open Access Journal, Peer-Reviewed, Refereed Journal Impact Factor 8.14 Calculate by Google Scholar and Semantic Scholar | AI-Powered Research Tool, Multidisciplinary, Monthly, Multilanguage Journal Indexing in All Major Database & Metadata, Citation Generator
Publication Details: Published Paper ID: IJRTI2604017
Registration ID:211086
Published In: Volume 11 Issue 4, April-2026
DOI (Digital Object Identifier):
Page No: a129-a137
Country: Hyderabad, Telangana, India
Research Area: Engineering
Publisher : IJ Publication
Published Paper URL : https://www.ijrti.org/viewpaperforall?paper=IJRTI2604017
Published Paper PDF: https://www.ijrti.org/papers/IJRTI2604017
Share Article:

Click Here to Download This Article

Article Preview
Click Here to Download This Article

Major Indexing from www.ijrti.org
Google Scholar ResearcherID Thomson Reuters Mendeley : reference manager Academia.edu
arXiv.org : cornell university library Research Gate CiteSeerX DOAJ : Directory of Open Access Journals
DRJI Index Copernicus International Scribd DocStoc

ISSN Details

ISSN: 2456-3315
Impact Factor: 8.14 and ISSN APPROVED, Journal Starting Year (ESTD) : 2016

DOI (A digital object identifier)


Providing A digital object identifier by DOI.ONE
How to Get DOI?

Conference

Open Access License Policy

This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License

Creative Commons License This material is Open Knowledge This material is Open Data This material is Open Content

Important Details

Join RMS/Earn 300

IJRTI

WhatsApp
Click Here

Indexing Partner