Beth, the Mars project--even if only built on the ground during testing--should give some good data for the intended use of the technology, which the website states is emergency and low-cost shelters and/or permanent housing, ads well as commercial buildings. It will be interesting to see the results.
The idea of being able to 3D print whole buildings is definitely something that could have huge impact on housing the developing world or even providing respite after disasters like the Japanese earthquake and tsunami and the earthquake in Haiti. I would think it's a fast, reasonably inexpensive way to get shelter up and usable quickly. I hope that this actually can become a reality because the possibilities are pretty unbelievable.
Jim, thanks for that experimental info. I've read elsewhere that one big inhibitor to date for using AM techniques in aerospace is the lack of resistance of the materials to temperature extremes, especially high temps. OTOH, high-end AM materials are not just for making prototypes anymore--they're increasingly used for low-end aerospace production components, as we've covered here http://www.designnews.com/document.asp?doc_id=236261 But since Stratasys' FDM is being used on test parts for Mars rovers, NASA must believe it's possible to overcome those limitations. Also, other materials have worked successfully on non-interior aircraft parts, usually processed with various forms of SLS.
To me, the most amazing thing is that this technology could be used to build "infrastructure, such as roads and landing pads." It's one thing to build components that have to handl light mechanical stresses. It's another to build structural components that have to handle big loads.
My initial thought about using the prototype materials was the thermal risks; meaning brittleness and prone to shattering in the extreme cold Martian temperatures. But I recalled a recent environmental test done to an SLS prototype housing. It was placed in a cold chamber at -55°C and an impact test was run, simulating a sharp impact at extreme cold. The housing was designed with a 2mm wall thickness, and the SLS didn't even dent, let alone shatter. And while Martian climate can exceed -55°C, that was the lowest limit of our chamber's capability. But I'm convinced; at least for SLS.
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