The two critical aspects, when it comes to verifying thermal analysis, are the model discretisation and idealisation and the reliability of material and geometrical data. As a result, the geometry construction of 3D thermal models is critical.
For every project that requires the design of complex systems such as satellites, small satellites, instruments, antennas, thermal engineers must build simulation models to
There are four main ways of building the geometry of thermal models (GMM):
Which methods you will choose among the four of them to build the geometry of the thermal model will depend on your needs. The most common way to build the geometry of thermal models in most cases is the geometry simplification from CAD models (STEP files) because you retrieve a lot of existing geometrical information such as the coordinates of the construction points of the geometrical shapes as well as the transformations that have been applied to them (translation, rotation) directly from the CAD models so you don’t start from scratch. Learn How to do a satellite from scratch with the Nitrexo's AI Digital Engineer
The radiation is critical for space applications:
From a thermal point of view, the radiation is critical for space applications as we have previously seen in how-to-efficiently-integrate-thermal-space-analysis-models.
The radiation mostly depends on surfaces area, so the surfaces must be modelled precisely in the thermal models. Geometry of small elements from the CAD files such as rounded edges, small holes, fillets, fasteners, nuts, and bolts do not significantly affect the final temperature results because their surface area is very small as compared to the surface area of the overall system.As a result, they can be neglected from the radiation point of view.
For space applications, the assumption of thin shell is often made. Satellite structural panels, antenna and instrument structure, solar panels count for the biggest surface area of the satellite. Their thickness area is small as compared to their main surface area so it can be neglected from the radiation point of view as well.
The process of simplifying CAD models (STEP files) for thermal analysis can be split into seven main steps:
Benefits: Defeaturing tools include several automatic functions to rapidly simply the CAD model, more control over the decisions.
Limitations: Built on user-defined basis, time-consuming and error-prone.
Standardizing the geometry construction process will reduce both time and computing which affect the product development budget, as well as the risk. .
We will standardise and fully automate this process and make it accessible to the entire space thermal engineers’ community via our Digital Engineer® Try it now