WARNING: this was a lot longer and 'scattered' than I recall, apologies in advance.
DISCLAIMER: This was a casual talk and I casually took some notes, and it happened over three years ago as of this writing. In short, don't assume anything below is an accurate representation of what Jinnah said. As a long-time SpaceX fan, and as a much longer-time software engineer, I was super pumped during the whole talk, and was definitely not focused on accurate recording.
https://www.realms.org/spacex-talk-notes.html
PS: I know most of this veers way off topic, but for some reason I decided to take this opportunity to share this material.
PPS: The comment was too long to post, so you'll need to click the above link. Sorry about that. If someone would like to distill the on-topic parts into another comment, that would be fine.
> They saw that at NASA. Because of the handoff, it caused them to push reliability ratings way higher than needed, which added complexity and customization.
Very interesting!
also
> it took Elon six weeks to go from "OK let's land on a boat" to actually having a boat. The software VP guy didn't think it 'was a 2014 problem...definitely 2015'...people who had been there longer knew Elon would be able to get a boat quick. Definitely a 2014 problem.
then this
> So then they'd fly balloons off of the boat so they'd get low level wind data, said data would go to the vehicle and be used for control for the last few km.
So many gold nuggets. Thank you!
You're welcome! I'd forgotten most of this and so it was really fascinating reading over it again just now, especially in light of all that SpaceX has been doing over the past 3.5 years.
>Facebook got jammed up because they had to re-write a lot of software under DO189B/C.
I typed this up 3.5 years ago, and didn't give a crap about Facebook one way or another at that time, so whatever was said there didn't stick with me at all.
Hopefully somebody else where can somewhat decode mystery string (that might have typos) based on context.
The CRS-10 that fly to the ISS seem to use RadHArd Cortex M4 or M0, according to this ARM PR document:
https://www.arm.com/blogs/blueprint/arm-rad-hard-chips-space
You can start poking around here: https://www.nasa.gov/content/commercial-lunar-payload-servic...
There's actually quite a few options in the "next gen" space, as many observed the need for updated compute. The one I've been closest to is HPSC: https://www.nasa.gov/directorates/spacetech/game_changing_de...