So Saf-t.. If I'm reading right, your 2 big reasons for not liking it is:
1: That it will deflect more easily (about 3x as easily)
2: SCC and also general fatigue
1 is somewhat mitigated IMO in that it will have to sustain almost 50% more force to reach yield (plasticity).. Yes, it'll deflect, but it won't stay that way until you hit something BIG.. big enough to have destroyed that .500 DOM a loooong time ago. But it *should* sustain multiple hit that would yield the DOM.
2: Nothing I can say other than what's the life expectancy of a lower link on a rock buggy no matter what the material? (Jim, Scott, Greg, shaddup..i can hear you already "As little as Rich wheels, a lifetime!"
) 1 year, 2 years MAYBE? I would be very surprised if SCC would play a role by then, considering a prime example I ran into while doing research was the landing skid on a Huey..
Average airframe prefix I remember seeing was mid 60's. Stored outside primarily, flown for thousands upon thousands of hours, and flexed every time it lands... Shit, they let ya do auto-rotations to the ground in those.. (Blackhawks will auto-rotate, but the landings aren't very kind to the airframe or occupants - no auto's to the ground in a 60)
Just because I don't have a degree from a technical university doesn't mean that -
A: I don't know what in the hell I'm talking about.
B: I don't know people that DO know what the hell they're talking about, (both MIT engineer-types and real-world usage types)
C: I don't know how to do research.
D: I don't weigh the pros and cons.
How's this:
DISCLAIMER TO ANYONE FOLLOWING THIS:
Aluminum links will NOT last as long as as steel link. It will fatigue over time, and may break, killing you, your family, and possibly a busload of nuns. If it doesn't brealk, it will likely deform upon impact. Whether it springs back or not is a function of a multitude of factors beyond this discussion.