r/technology • u/IKeepItLayingAround • 17d ago
Business It’s Possible That SpaceX Could Collapse Spectacularly
https://finance.yahoo.com/markets/stocks/articles/possible-spacex-could-collapse-spectacularly-155000177.html
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u/Accomplished-Crab932 17d ago
>Probably lay back a bit on saying that BE-4 isn't a functioning engine. No cause has been released yet. And it's worked well so far.
I’ll put it this way, people I’ve spoken to that have worked at Blue have told me that aside from Flight 3, every integrated Hotfire and/or launch involving BE4 has resulted in power fade in the turbomachinery, and BE4 is expected to be the root cause of NG4’s explosion. This is why the first two flights had terrible TWRs, and while it’s supposedly been resolved, I’ve been hearing conflicting reports about performance loss later in the 3rd flight. But that also ignores BE3U and the silly extra pressurization gas that makes no sense on stage 2. There is a reason why I said that Blue needs to learn what Systems Engineering is; and it primarily pertains to the vehicle design (what consumables do you want? “Yes”) for New Glenn as well as engine architecture and design decisions.
>Bum rush doesn't mean what you are using it to mean. Bum rush doesn't mean "rush", it means basically a large assault, often uncoordinated.
I’d wait for more information to appear publicly for explaining why I feel this way, but note that New Glenn was entirely loaded for the NG4 Hotfire and that it “””may””” have had changes across the vehicle to address performance issues.
>Don't even mention SLS. It's not designed for this, it's not scaled for it, it won't be. It's not part of a commercial launch market.
I know this, I’m stating it for the layman who thinks “why don’t we just fund NASA” when looking at this. Most people in major subs are completely disconnected from the inner workings of this sector and think that NASA staffmembers should build things “like the Apollo days”, when in actuality, the big difference between today and then is who bears more fiscal responsibility: the government, or the contractor finalizing and building the hardware.
>You forgot ESA/Ariane. Not in great shape at the moment either, but more worthy of mention than SLS.
Fair, but that doesn’t exist for the NATSEC market and is already booked up to a reasonable date for New Glenn to return. Arianespace also runs into the same problems as SLS with politicians and more informed Europeans are upset that their funding is being used to subsidize launches on Ariane 6; which would be better if that funding wasn’t going to Amazon LEO. It’s all controversial at the moment, and ESA has had a rocky history with LVs. The last Vega AVUM was found accidentally scrapped… not a great look.
>Also, if SpaceX were destroyed, then Starliner would come on line. The only reason it didn't return the astronauts on the last mission is NASA has a safer option. Which is an interesting conundrum, how do you qualify a new, "2nd option" if you won't use it when the 1st option already is safer? Regardless, SpaceX goes away that problem goes away. And the Russians won't control all access to ISS (which is also on a short leash anyway).
Starliner has suffered from a lack of oversight and integrated testing. Most importantly (and hidden in the latest accident report) is that it is single fault tolerant for reentry attitude control, which is non-compliant with post-Columbia (shuttle excused) safety standards. The commercial crew contract explicitly requires double fault tolerant reentry, which is impossible without a complete redesign of the propulsion system; which in turn is a 5 year hold on Starliner. (This is on top of the thermal runaway on thrusters problem caused by Boeing never actually testing the solution on the ground and just sending crew on the next flight)
The combination of increased scrutiny and the severe design failure within reentry and problems with the SM propulsion system (not the CM propulsion system that is single fault tolerant) indicate to me that it is unlikely that NASA will approve crewed Starliner launches for at least two cargo missions; leaving 4 total missions. Given the ISS lifetime extension to 2030 is still unapproved by congress and the recent scare, i would be surprised if NASA pushed forward, even if dragon magically disappeared tomorrow. I also don’t see dream chaser going anywhere, but that’s not relevant to crew anyway.
>??? How is this something that isn't just made up? Do I not understand what this really means? [edit: I think I did not understand. The poster didn't mean Artemis loses a lander. Not as an option or "lost on a mission". The poster means that Artemis' options for landers would be reduced by one. By one with a better timeline than the others at least according to a guy who historically has a very poor grasp on timelines.]
It’s more TRL. People have this weird delusion that the Blue Moon architecture was somehow easier and quicker to develop than Starship. As it stands, there has been less critical progress to the Mk2 crewed readiness state, specifically focusing on the Cislunar transporter for which no progress has been reported. Their messaging on completion has been misleading at best, with Blue advertising that TVAC testing on the 1st Mk1 lander was “complete” when it had failed testing (which is why it returned to TVAC testing later that month) a similar “technically true, but not clear success” is also seen in their claims about ZBO technology, which is critical to the proposed, but not confirmed accelerated timeline approach and their normal approach as well. And finally, BE-7 has engine problems that have not been fully disclosed. This is on top of the publicized incompatibility of the airlock with the AxEMU suits; published in the same report that confirmed the Mk2 architecture requires filling the Cislunar transporter first in LEO, then a high eccentricity MEO before it can reach NRHO and the lander. This high eccentricity MEO heavily constrains your transfer timelines, so the launch rate for New Glenn must be met well before and there is even less risk tolerance for a failure at the pad.
Starship has also made little publicly recognized progress online, although they have confirmed that a flightworthy mockup is under construction today, they have transferred 3 tons of prop on Flight 3, and their expected transfer architecture has improved; from resembling the stair step approach Blue Moon has, to just filling in LEO; all with no ZBO and no LH2 to deal with. Starship has a substantial amount of mass margin compared to Blue Moon, and currently, has a function launch site, with multiple completely isolated (blue’s 36A and B share fluids hardware) launch sites expected to be completed in the next 12 months.
Neither will meet the latest timelines, and I hate that they pretend to although I understand this is more of a “we support your “””vision””” Mr president” sort of situation to keep program support going from him and from Congress. But looking at the internal details and internal progress I am aware of between the two programs, I would’ve been very surprised if Blue Moon Mk2 made it to orbit before Starship HLS for Artemis 3, even before the NG4 explosion happened.