Master Thesis - OUFTI-1
Master Thesis - OUFTI-1
Master Thesis - OUFTI-1
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Figure 3.9: Classication by density and yield stress<br />
So, the nal classication of these materials is:<br />
1. CFRP<br />
2. Al alloys<br />
3. GFRP<br />
4. T i alloys<br />
However, an other important criterion to take into account is the cost. Indeed, each of<br />
these materials has a given cost, which is not the same for each of them. Moreover, the<br />
cost is also closely linked to the manufacturing process which can be used to modeled the<br />
material into the desired form.<br />
For this reason, Al alloys become more attractive than CFRP. In addition, the choice<br />
of Al alloys allows to create a support with more restricted dimensions, which is really<br />
important considering the available space between EPS and xEPS cards.<br />
The selection of a particular alloy was then based on an ESA requirement which stipulates<br />
that: "Aluminum 7075 or 6061 shall be used for both the main CubeSat structure<br />
and the rails. If other materials are used the developer shall submit a Deviation Waiver<br />
Approval Request (DAR) and adhere to the waiver process ".<br />
In this requirement, the denition for a "CubeSat main structure" is the following one:<br />
a main structure is a structure which supports, in addition to its own weight, the weight<br />
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