It does though. During the development process. SpaceX will do five launches with lower reliability vehicles before the big launch providers will even do a single launch, and those five will have be cheaper in total. Of course, they aren't putting essential cargo (or god forbid people) on these higher risk test flights. By the time they're doing that they have developed certainty in the design.
A number of Tesla-related deaths can be attributed to Autopilot malfunction. Real people - really dead.
Except Tesla, unlike SpaceX, is willing to put passengers in its test vehicles. The SpaceX approach would be to let a bunch of FSD Teslas crash into things and each other before giving them payloads.
Citation needed. Not Tesla's "stats" that if the people compiling them completed anything more than high school statistics are intensely misleading.
Comparing a subset of miles driven on the simplest and easiest roads (because the systems can't be used and are turned off) and comparing to accident stats across ALL roads is disingenuous to the extreme, and Tesla continues to tout it.
Short of pulling over, humans don't have the opportunity to say "let's disengage, because it's a bit challenging", and then not have to worry about "counting" any accidents from there forward.
SpaceX does not have a difference in intended reliability, or a difference in design reliability. (At least for the rocket as a whole. One could argue that 33 engines allows lower engine reliability through redundancy)
What they DO have is a significant difference in prototype reliability for live launch. This is clear when you look at their launch history.
I don't think that is accurate. There is a difference between 9%, 99%, and 99.999% confidence of success going into a launch.
You can almost always delay builds and launces to run more simulations, tests, and studies and increase confidence.
A simple example is SpaceX could have chosen to wait until they had a booster test with 100% engine ignition before moving on a full launch. Instead they choose move forward anyways without more stationary booster testing.
Why? If you're launching people I see why you want near-perfect, but if you're launching something with a low replacement cost (ex: getting fuel to orbit to support other projects) it seems to me that as volumes get large enough eventually "use lower quality and accept a slightly higher probability of failure" starts to be cost effective.
Your comments in this thread all go against the development approach of that rocket— Falcon9 is a stable platform now as it is used in production. In the development phase there were tons of explosions. This all happened in the past.
Is unarguably cheaper to forgo the additional testing and cost required for human flight.
But this is totally false. There are entirely different standards applied if you want to design an aircraft for commercial airline passenger transport vs for general aviation. There are entirely different requirements for instrumentation reliability if you're building a day-VFR aircraft vs one that is allowed to fly in instrument conditions. And there are entirely different requirements for aircraft that you sell to the public vs ones that you build yourself.
The aviation side is full of examples of exactly the sliding scale you're saying doesn't exist.
Of course there is. The famous example is radiation hardening. SpaceX opted for redundancy instead. Not only cheaper, but more modern, too.
> in such as complex high-energy environment, there is no money to be saved by building less-than-perfect machines
SpaceX has launched zero humans. (EDIT: Totally wrong!) It aims to, so target reliability is high. (I would argue their track record in production is a product of their willingness to push the envelope in tests.) But there is a large market for cheap, if unreliable, launches. Because there is an emerging market of cheap satellite makers.
It is the only US entity with the capability to do so.
Sorry, had a brain fart, no idea how I typed that out.
Indeed, if we assume that the each launch is an IID binomial coin flip (which isn’t really the right way to evaluate right-censored data), and observe (by reading Wikipedia) that SpaceX has had at least 450 successful Falcon 9 launches since the last in-flight failure, then they have at least five nines of reliability:
0.999995^450 ~= 449/450.
Which appears to be an industry-leading stat.
For context (excluding the Columbia re-entry failure), the space shuttle only had 4 nines:
0.99994^125 ~= 124/125
I saw in another comment that each SLS launch costs $2B. Do you think SpaceX spent $2B on this launch? I find it hard to believe.
substitute rocket and spaceflight with airplane and flight and see how that sounds
Yes ultralights have some regulations, but even general aviation has less regulations resulting in cheaper aircraft, to say nothing of ultralights.