• Devi prasanna kakarla
• Antony Binu Stheyban
• Rakesh S
• Jangam Hemanth
• Gaddam Vinay

The article is regarding the analysis which has been done on the Design and Fabrication of Atmospheric Sensing CubeSat. The cause of aiming the project is easy to construct and cost-efficient to fabricate make clear for students at the graduation level for doing capstone projects. By investigating this paper one will incur construct the CubeSat and understand the factors that should be scrutinized while designing or studying CubeSat. The study will present from the structure design constrain to payload constrain. With the ESP board connecting with these sensors followed by DHT 11, GPS sensors (NEO-6m), Gyroscope (L3G4200D), and Ultrasonic (HC-SR04) were used with the intention of extrapolating the database. Introducing efficient design with preferable structural analysis. The Acrylic sheet is used to have superior strength to the CubeSat and the properties of the material are also mentioned in table no.1. Monoacrylate Solar Cells are used to charge the battery naturally. Sensors are connected to get data from satellite-like temperature, humidity, the position of the satellite, movements of satellite, and obstacle distance. 2 cells of 7.4V 30C having 360 mah battery are used. The Brushless fan is used for air intake.

CubeSat, ESP 32, DHT, Ultrasonic Sensor, GPS, Gyroscope, Atmosphere

"Design and Fabrication of Atmospheric Sensing CubeSat using Acrylic Sheet", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.12, Issue 7, page no.g80-g86, July-2025, Available :http://www.jetir.org/papers/JETIR2507620.pdf

"Design and Fabrication of Atmospheric Sensing CubeSat using Acrylic Sheet", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.12, Issue 7, page no. ppg80-g86, July-2025, Available at : http://www.jetir.org/papers/JETIR2507620.pdf