Hi all,
I'm performing a thermal analysis of a satellite subsystem (antenna). However, I'm having some issues relating to the model that I'm implementing on ANSYS.
I've already computed the values for the solar flux, albedo and IR that the satellite is subject and I've applied it to different...
I'm working on an university project to developed a reaction wheel for a cubesat.
After defining that the minimum generated torque for the RWS is 8.8e-6 Nm and that the reaction wheels shall be able to hold an angular momentum of 4.82e-4 Nms (around the Z axis), I start computing the systemic...