> 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
I’m not a rocket scientist, but then neither is the author.
Are you sure about that?
https://spaceflightnow.com/2022/05/24/spacex-swapping-heat-s...
Anyone know if there's a detailed response from NASA to the article?
"countdown clock started ticking down" "to a targeted launch time of 6:24 p.m. on Wednesday, April 1."
The only thing the author of this blog piece has to offer that’s new is his very strong personal intuition that the new design hasn’t been properly validated, without any engineering explanation about why the testing the performed won’t adequately simulate real world performance.
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/
Fun wording. This isn't news, concerns have been raised about Artemis II saftey in the past 3+ years since Artemis I and before then as well.
>> Artemis II could fly just as easily without astronauts on board
Is Orion’s heat shield really safe? New NASA chief conducts final review on eve of flight. https://arstechnica.com/space/2026/01/nasa-chief-reviews-ori...
> 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.
johng•1h ago
jojobas•1h ago
everyone•1h ago
evan_a_a•1h ago
everyone•1h ago
I didnt know, cus I just dont give a shit about this stupid project.
wat10000•38m ago
Of course, six decades later, we should be able to do a lot better.
saghm•1h ago
tonymet•58m ago
cr125rider•1h ago
jaggederest•1h ago
fishgoesblub•41m ago
paleotrope•31m ago
idlewords•24m ago
There are rumors (that I've never been able to run down) that the astronaut corps insisted on this so the Shuttle could not be flown unmanned.
steve-atx-7600•1h ago
bch•1h ago
tonymet•59m ago
mikelitoris•53m ago
shrubble•46m ago
wat10000•41m ago
1shooner•38m ago
Columbia and Challenger crew totaled 14, who else are you referring to?
staplung•30m ago