The reason he was tinkering on small engines in his garage instead of designing big engines for his employer, TRW, was that after designing the best American first stage engines (the TR-106 and TR-107), it became clear that it didn't matter that his engines were better, for political reasons it was impossible to kill the RS-25 program (also known as SSME, or Space Shuttle Main Engine), and therefore any future vehicle would use them instead, despite them being strictly worse for any use other than for the Space Shuttle. This was immensely demoralizing to him, and he was considering just quitting the industry and doing rockets as his hobby. Then Musk managed to convince him to work at SpaceX, for a much lower wage (and stock options, but the rational early valuation for rocket company stock is $0), mostly on the promise that at SpaceX, his engines would actually fly.
The NASA program of record heavy lifter, SLS, is still using the designed-in-70's RS-25 now, 25 years later, and plans to toss 4 of the $40M engines into the ocean on every flight. SpaceX is what happens when you build rockets with actually modern technology, instead of all the components NASA is forced to use because some senator needed to maintain employment in his home district.
NASA did no such thing. They were ordered to use the engine by the Senate.
(When the Constellation program was canceled and the SLS program was created, Senate ordered NASA to pick solutions that "minimize contract cancellation costs". Not minimize total costs, minimize costs related to cancelling contracts. This of course means that the contractors you are already using can offer any solution they want, at any price they want, and so long as they are willing to waive the contract cancellation penalties as part of their package, you have to pick that solution.
They all offered a really expensive, really bad deal. I know several NASA engineers who quit in disgust because of this.)
Even when dedicated non-military rockets began to appear, e.g. the Ariane range and the Space Shuttle, they had dependencies on legacy infrastructure that was originally designed for strategic weapons (i.e. it was intended to work at peak performance, just once). The payloads evolved to reflect the launch system constraints, so very expensive, one-of-a-kind comsats and earth resources satellites, each of them a bespoke design (or at most one of a dozen or so).
SpaceX isn't building missiles; it's optimizing for reliability and cost (which means reusability). More like airliners than missiles. This doesn't mean low performance (the efficiency and power density of a modern civil airliner turbofan would have been a jaw-dropper to 1940s military aviation engineers) but it does mean the performance goals are different.
I am still extremely skeptical that Heavy/Starship will facilitate a Mars colony ... but that's because I'm skeptical about the economics and practicalities of building an off-planet colony when the externalities we normally take for granted (like a compatible biosphere) aren't available and nobody's really done the necessary R&D work on self-contained biospheres -- even the ISS is effectively an open-loop system dependent on constant resupply. (Biology and ecology are much harder than they look to a naive outsider.)
Neal Stephenson has a pretty good article about path dependence in space exploration: https://slate.com/technology/2011/02/space-stasis-what-the-s...
I wouldn't be surprised to see a small settlement for research or something in my lifetime. Maybe something like what we have in Antarctica.
The next step would then be something like a Bigelow B330 module in LEO, which is close enough to get the astronauts home from in a hurry if something goes badly wrong.
(These steps can be commenced with current tech: Heavy/Starship not required.)
Step 3 would be a bigger test hab out beyond the Van Allen belts, preferably a couple of habs revolving around a hub to provide centrifugal "gravity" at Lunar or Martian levels. Goal is to test systems for use on planetary surfaces exposed to cosmic/solar radiation (because outside our atmosphere). Starship is probably mandatory for this phase, because it's a lot more massive and a lot further away. Alternatively: conduct this experiment on the Lunar surface, once astronaut return capability is available (but why waste expensive reaction mass if you can simulate a gravity well?)
Without a lot of R&D work under these conditions, a closed-circuit life support system for Mars is a huge safety risk for the astronauts who set it up (and who are too far away to rush home in a hurry if it goes badly).
And without closed-loop life support, a Mars "colony" is no more a colony than an Antarctic research station reliant on resupply for everything except air and water.
Also his system strategy is : the best design to use is one that doesn't require the design in the first place. Ie get rid of many systems. Keep it simple. Less can go wrong, and the schedule is reduced. "Tight is right. Long is wrong". He did a great talk last month.
You guys might like a video I'm releasing on Halloween, "the actual, physical, reason why time slows at the speed of light". My channel is "TheRainHarvester". Stay tuned...
from wikipedia "In late 2001, Mueller began developing a liquid-fueled rocket engine in his garage and later moved his project to a friend's warehouse in 2002.[1] His design was the largest amateur liquid-fuel rocket engine, weighing 80 lb (36 kg) and producing 13,000 lbf (58 kN) of thrust.[1] His work caught the attention of Elon Musk, PayPal co-founder and CEO of Tesla Motors, and in 2002 Mueller joined Musk as a founding employee of SpaceX."
that's a hell of a lucky find by Musk and a hell of a roll of the dice by Mueller. Around the same time is when Shotwell joined, she's equally incredible but in a different way. i don't now how Musk found her.
Even then, what followed has been black swan territory. Every major development announcement at SpaceX is met with "you're crazy" and laughter from the industry and yet, a few years down the road, there it is working. Again, i really want to know what went so right.