Stuff for GSM/CDMA has been around for years, OpenBTS is the primary example. This is the first I've heard of anything more modern/complicated being implemented. From my understanding, a lot of the hard eng work is in the RF frontend and making it small/low power enough to fit in a phone for example. OpenBTS got around this by using existing SRDs for their RF frontend.
Working in the government space sector, generally speaking, you're given a mission lifetime which is seen as a minimum. your payload/spacecraft/instrument needs to last at least this long. some things end up being limited by the physics of the system (See the RTG on the Voyager probes for a common example, or CEMs on plasma spectroscopy instruments for a more obscure example). However, in pretty much all cases where the physics doesn't put a hard cap on the thing you're building, nobody wants the thing building to be the first thing, or critical point of failure of the whole system.
jval43's quote puts it pretty well. It's not just that you're designing something to last, you're designing it not to fail. It also tends to help when you have a bunch of really smart folks from a number of disciplines working on the same problem.
With that said, you need to walk a fine line as far as the level of redundancy and fallbacks you put in place versus the overall SWaP (Space Weight and Power) of the system. I can go somewhat deeper into SWaP issues if you would like.
I can't seem to find a reason for shutting it down in the article. Does anyone have info on this? Was it for budget reasons or was their a failure on orbit?
As someone who specializes in the type of low level systems that are still built in C, C++ is considered high risk let alone rust. That is largely the reality of the industry. Some co-workers and I hope to introduce C++ as an experimental project next year. We also have some data processing code written in C++ that we would like to integrate as is. The reality on the ground is that C is often used over C++. ¯ \ _ ( ツ ) _ / ¯
The Ingenuity is a really interesting project with some important lessons for spaceflight with unhardened CotS parts. However, I would argue that it and the Europa Clipper are two very different designs for two very different environments.
While mars is an elevated radiation environment when compared with earth, the Jovian radiation belts are on a whole other level, particles up to 1-2000 MeV are fairly common. To put that into context, a medical radiation beam therapy deals with 2-300 MeV on the absolute highest end. To get into the 1-2000 MeV range you generally are talking about energies found in the low end of particle accelerators. Ingenuity mostly had to worry about Total Lifetime Dose (TLD), one example of a TLD issue is dopant migration induced by high-energy heavy ion collisions which can change the on voltage of a transistor. At high energies you can have single events with enough energy to cause fatal latch-ups. For instance modern rad-hard FPGAs start encountering major issues around 60-70 MeV.
Furthermore, these parts are power MOSFETs which control power for whole subsystems so their reliability is critical to the operation of the spacecraft. In addition, the biggest issue here is not just that there were issues that were addressed and fixed, it's that Infineon didn't issue an errata to the datasheet or inform NASA of the issue. As a result there are now transistors littered throughout the spacecraft which don't meet the radiation needs. This is going to require reworking the boards, re-validation of the subsystem, and re-integration of the subsystem into the spacecraft. This all comes at a non-trivial impact to budget and timelines which is to say nothing about what this does to the launch window the project was trying to hit for gravity assist / proximity.