The Age of Asteroids
newyorker.com
newyorker.com
The RAD750 is based on a 1996-era PowerPC design, so the statement is technically true, but as far as I know it's basically the state-of-the-art in rad-hardened processors -- it's the same processor used in Boeing's 787 FMC, for example. (SST did just ship a rad-hard M0, which is kind of neat.)
Lewicki's not just talking off-the-cuff here -- he's one of a few people actually qualified to opine on spacecraft engineering -- but I wonder, what does he think should be used in place of the hugely-expensive, arguably-antiquated but undoubtedly robust systems currently in use?
This gap makes it possible to take risks and use newer hardware, specifically hardware that has not been radiation-hardened or even tested in orbit.
Normal CPU's don't last long enough in space to be all that useful for satellites. And even for profit telecom companies stick with radiation hardened CPU’s so it's not like this is a case of 'military' over engineering.
So, what's Mr. Lewicki's alternative?
When you are sending a suite of purpose-built instruments and a one-of-a-kind rover to Mars, taking advantage of a narrow launch window, to accomplish a very well-defined scientific mission, you require the spacecraft to be safe.
If you are sending a bunch of less-expensive spacecraft to perform a less intensive investigation of a bunch of asteroids, you might be more risk-tolerant. But as the cost of the instrument suite goes up, you'd have to be more risk averse.
Additionally, if you expect to be in a difficult radiation environment, things change. LEO is not a difficult environment, but deep space is.
It's a systems engineering problem, and there is no single correct approach. It's an engineering question, with the usual set of tradeoffs, expertise, and modeling. NASA and private industry have been studying this for decades now. (I spent a couple of years working on a software-implemented fault tolerance scheme for science algorithms in spacecraft.)