Artemis II is not safe to fly
https://idlewords.com/2026/03/artemis_ii_is_not_safe_to_fly.htm
Artemis II is not safe to fly
https://idlewords.com/2026/03/artemis_ii_is_not_safe_to_fly.htm
This is a concerning read, I'm not quite sure what the driving motivation is for Artemis, but the following answered at least part of my question -
> That context is a moon program that has spent close to $100 billion and 25 years with nothing to show for itself, at an agency that has just experienced mass firings and been through a near-death experience with its science budget
> “Our test facilities can’t reach the combination of heat flux, pressure, shear stresses, etc., that an actual reentering spacecraft does. We’re always having to wait for the flight test to get the final certification that our system is good to go.”—Jeremy VanderKam, deputy manager for Orion’s heat shield, speaking in 2022
This is a strange claim, considering NASA used to have 2 facilities that were capable of this - one at Johnson and one at Ames. They were consolidated (https://ntrs.nasa.gov/api/citations/20160001258/downloads/20...) but it seems like the Arc Jet Complex at Ames is still operational https://www.nasa.gov/ames/arcjet-complex/
By having a much higher launch cadence and then analyzing the flight hardware afterwards.
Also, they don't have anything human rated going beyond LEO. Coming back from the moon means you're going significantly faster and thus need a better heat shield
> I am very not brave but I'd volunteer.
>> Artemis II could fly just as easily without astronauts on board
I haven't kept up with Artemis development but I've read extensively about Challenger and Columbia. These two parts of the article stood out to me:
> Moon-to-Mars Deputy Administrator Amit Kshatriya said: “it was very small localized areas. Interestingly, it would be much easier for us to analyze if we had larger chunks and it was more defined”. A Lockheed Martin representative on the same call added that "there was a healthy margin remaining of that virgin Avcoat. So it wasn’t like there were large, large chunks.”
Followed by:
> The Avcoat material is not designed to come out in chunks. It is supposed to char and flake off smoothly, maintaining the overall contours of the heat shield.
This is echoes both Shuttle incidents. Challenger: no gasses were supposed to make it past the o-rings no matter what, but when it became clear that gasses were escaping and the o-rings were being damaged, there was a push to suggest that it's an acceptable level.
There was a similar situation with heat shield damage and Columbia.
In both cases some models were used to justify the decision, with wild extrapolations and fundamentally, a design that wasn't expected to fail in that mode /at all/.
I know the points that astronauts make about the importance of manned space exploration, but I agree with this author that it seems to make sense to run this as an unmanned mission, and probably test the new heat shield which will replace the Artemis II design in an unmanned re-entry as well.
About the last point:
At this point in time, manned space exploration should come out of our entertainment budget. The same budget we use for football or olympic games.