Development Of A Deployable 3u Cubesat Solar Panel Array

The solar panel is mechanically constrained by tightening the nylon wire through the mechanical hole interfaces on the solar panel as shown in figure 1.
Development of a deployable 3u cubesat solar panel array. Developed a burn wire triggering type of mechanism for deployable solar panels for 3 u cubesats called micromas. Design and development of cubesat solar array deployment mechanisms using shape memory alloys. High resolution 1m 10km swath 3u cubesat concept. Good power management is also vital to maximise efficiency and safety on board.
The gaas solar array and m6p solar panels by nanoavionics the nanoavionics gaas solar arrays and panels are made of high performance triple junction space grade solar cells for missions with high power requirements. It supports multiple integrated sensors and it is fully compliant with the cubesat standard. The high power generation capabilities radiation and temperature resilience ensure smooth space operations. Several deployable solar panel solutions for 3u cubesat have been developed with total delivered power ranging from 22 w to 56 w e g.
Tailored solar panel configuration to match orbit mission is more important than solar cell area. Allen guzik and othmane benafan. Our 3u solar panel x y utilizes seven highly efficient triple junction solar cells. 3u cubesat solar panel equipped with 7 solar cells providing up to 8 43 w per panel in leo.
Several deployable solar panel solutions for 3u cubesat have been developed with total delivered power ranging from 22 w to 56 w e g increasing the performance with respect to body mounted solar panels from 160 to 400.