Design and Development of the Satellite Structure and The Aentenna Deployment for the 1u CubeSat
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
Authors
- M Saravanan
- Manish R. Patel (ORCID: https://orcid.org/0000-0002-8223-3566)
- Harshit Katnoria
Publication Details
- Journal
- International Journal For Multidisciplinary Research
- Published
- 2025-05-10
- DOI
- https://doi.org/10.36948/ijfmr.2025.v07i03.44339
- Primary Topic
- Spacecraft Design and Technology
- Type
- article
- Field-Weighted Citation Impact
- 0.00