International Journal For Multidisciplinary Research

E-ISSN: 2582-2160   •   Impact Factor: 9.24

A Widely Indexed Open Access Peer Reviewed Multidisciplinary Bi-monthly Scholarly International Journal

Call for Paper Volume 7, Issue 3 (May-June 2025) Submit your research before last 3 days of June to publish your research paper in the issue of May-June.
Submit Research Paper Join as a Reviewer

Plagiarism is checked by the leading plagiarism checker TurnItIn

Call for Paper

Volume 7 Issue 3
May-June 2025

Submit your research paper

Indexing Partners
Academia Advanced Sciences Index Bielefeld Academic Search Engine CiteSeer DRJI Google Scholar Independent Search Engine & Directory Network ISI (International Scientific Indexing) Issuu Mendeley Research Networks
RefSeek ResearcherId - Thomson Reuters ResearchGate Scirus Scribd Semantic Scholar UTeM - Universiti Teknikal Malaysia Melaka Wiki for Call for Papers WorldCat Zenodo

Design and Development of the Satellite Structure and The Aentenna Deployment for the 1u CubeSat

Author(s) Mr. Mehulkumar Nareshbhai Patel, Mr. Harshit Katnoria, Dr. M K Saravanan
Country India
Abstract Whenever we think of satellite the first thing that comes to our mind is big in size, requires a lot of fuel
etc which is very true. But if I tell you there are satellites whose size is just like a 3x3 rubik's cube and can
help in remote sensing ,communications and many more. These small satellites are known as CUBESAT.
This Paper presents the design of internal and external components of 1U CUBESAT.
This Paper also provides critique on the insufficient data present for lunar exploration. Finally the external
design of CUBESAT has been implemented on Fusion 360 with dimensions of 10cm*10cm*10cm and
Static stress, Vibration and Thermal analysis has been done in Simulation section of Fusion 360.Whenever
we think of satellites, the first thing that comes to mind is that they are large, require a lot of fuel, etc.,
which is very true. But if I tell you, there are satellites whose size is similar to a 3x3 Rubik's cube and can
help in remote sensing, communications, and many more things. These small satellites are known as
CUBESAT. This Paper presents the design of internal and external components of the 1U CUBESAT in
a systematic manner, and to better understand the configuration of the satellite, sensors like the MPU6050
and LIDAR have been integrated into the CUBESAT to get the orientation and surface examination,
respectively. This Paper also provides a critique of the insufficient data present for lunar exploration.
Finally, the external design of CUBESAT has been implemented on Fusion 360 with dimensions of 10
cm by 10 cm by 10 cm, and Static stress, Vibration, and Thermal analysis have been done in the simulation
section of Fusion 360
Keywords Aerospace engineering, Aeronautical Engineering, Satellite and Antenna Deployment
Field Engineering
Published In Volume 7, Issue 3, May-June 2025
Published On 2025-05-10
View / Download PDF File

Share this



E-ISSN 2582-2160
CrossRef

CrossRef DOI is assigned to each research paper published in our journal.

IJFMR DOI prefix is
10.36948/ijfmr

Downloads
Research Paper Format Copyright Permission Form and Undertaking Form Cover Page Vol 7 Isu 2Cover Page Vol 7 Isu 1Cover Page Vol 6 Isu 6

All research papers published on this website are licensed under Creative Commons Attribution-ShareAlike 4.0 International License, and all rights belong to their respective authors/researchers.

CC-BY-SA Open Access

About IJFMR
Fees & Payment
Current Issue
Publication Archive 		Submit Research Paper
Track Submission Status
Publication Guidelines
Publication Ethics
Peer Review & Plagiarism 		Join as a Reviewer
Editors & Reviewers
Reviewer Referral Program
Get Reviewer Membership Certi. 		Website/Journal Policies
Usage Policy
Content Policies
Privacy Policy
Contact Us +91-9687-828-838 editor@ijfmr.com