That's assuming the regulations are competent. But if you let the market consolidate then the incumbent has enough money to buy off the government. Or it happens the other way around and the government is kind enough to set out regulations that only a megacorp can satisfy, thereby destroying the competition and awarding the last company standing the vaunted "too big to fail" get out of jail free card.
Which in turn gets you the 737 MAX sort of problems where the regulations both cause a problem (recertification is prohibitively expensive) and then fail to impede the incumbent's efforts to shirk it because you can't be damaging the business of your only domestic producer.
Work for a company with lots of small contracts and you'll quickly see "oh the Navy does things this way, AFSOC wants it that way, DHS does it another way" and so on. Competition arises among the small companies because all these different agencies behave like independent buyers, even if they are all part of the same government.
The corruption issue is damped within the realm of small contracts, because it's hard for executive-level corruption to trickle that far down the bureaucracy. It's just hard to make a bunch of smaller organizations move in lockstep, even if they have the same top-level leadership.
Granted, network effects still matter. Certain groups want their stuff to be compatible with other groups' stuff. They all talk to each other too. If you bin a demo with JSOC and the guy has a buddy in AFSOC, you bet he's gonna get a beer with his friend and say "man, company X really binned it today." So there are still some consolidating pressures.
And you're right, all of this falls apart with the huge contracts. Just food for thought.
I know your comment was likely made as a knee jerk reaction to the above comment but I implore the reader to actually consider the process and incentives by which rules and regulations are created and how an assumption of good faith negatively affects the rules and laws we get.
A plane built for resilience against defective engine components would be very different from the airliners we fly today. I would assume more engines for redundancy, better protection against catastrophic failure, different designs to allow engines to function even if parts flew out, and so on. It’s an interesting design exercise to build from radically different expectations from the fundamental parts.
Alternatively, a far less radical redesign would be turbines running at a much more forgiving regime feeding electric motors.
Do you think todays aircraft are not designed with the idea that the engine can fail?
And if you have unreliable components do you think redundancy is going to save you?
And lets be real - there already exist a aerospace arena where you have a higher number of CAT-events - it's called the military. And they deal with it by having a parachute for each passenger..
No - in effect building jet-engines (that are commercially viable i.e. fuel and efficeny) is not a easy to disrupt business. And the cost of entering it would be - high. And the benefit, well less obvious.
Of course they are - but the engines are also designed to be extremely reliable, and that's why you get away with two engines on long flights over water, something previously only available for planes with four engines.
> No - in effect building jet-engines (that are commercially viable i.e. fuel and efficeny) is not a easy to disrupt business.
That's true. My point being that building a better jet engine might be the hardest way to disrupt the business - making a better propulsion system, which might or not include a jet engine, is a less difficult approach. If you have an electric plane with two motors, a big APU-like turbine charging a battery and powering the motors, you might get away with a cheaper turbine, running in less extreme regimes, and still have a more fuel efficient plane requiring less maintenance than a pure turboprop would.
You don't win a stacked game by playing it by the rules. You win by changing the game to another one you can actually win. China did that with cars already.
This works for hybrid cars because the power demand when driving varies widely, as does the output speed. The 'hybrid' bit gets huge gains by always running the engine at optimal rpm+throttle, and using the battery to cover peaks and absorb troughs (regen).
A plane cruises for many hours at a fairly constant speed and throttle, which is designed to hit peak efficiency of all components. The 'hybrid' design therefore falls far behind on weight, efficiency and cost.
This is why short-haul flight will be the first to adopt hybrid propulsion.
Used for getting between islands for example
For a hybrid system to be worth it, you need to claw back more efficiency than you lose in going from mechanical energy to electrical energy, and then back again. For cars, this is generally the case, because they're always accelerating and decelerating. Their wide operating band means that the engine will always be a game of compromises, which is why sticking a motor and battery in the loop and decoupling the engine from the wheels is beneficial. But planes aren't like that; they go from setpoint to setpoint, and they stay in a given configuration for long periods of time. They have very narrow, highly optimized operating bands, so hybridization just isn't as effective.
For short-haul you spend a lot of time climbing and descending in relation to long flights, so the plane spends less time at the optimum the engines were designed for (cruise), so, if the power unit can be at the peak efficiency throughout the flight, with extra energy being supplied by the onboard battery for take-off and the power unit be shut down for descent, we might get to a point where it's economically viable, depending on battery operating costs and weight.
You are right to point out the aerospace industry has tried everything conceivable to see what sticks, but technology evolution sometimes throws us a curveball.
And it's not like the industry has missed this possibility. I've seen papers on systems as exotic as combining high temperature fuel cells (SOFCs, PCFCs) with the Brayton cycle to achieve a hybrid powerplant. The bar for novel propulsion systems in aerospace is extraordinarily high, higher (imo) than it is for automotive. The exception is unmanned systems, which are new enough and varied enough that there's been an explosion of activity, which has been exciting to see.
Aerospace RND has been looking into hybrid propulsion systems for a long time. If there's one thing they aren't shy about pushing, it's the ability to go higher, faster, more efficiently. Such systems aren't used because they aren't yet good enough.
I'm not convinced that humans are particularly effective in emergency situations, especially when they're expected to go from monitoring systems that work 99.99% of the time, to suddenly aviating with alarms going off everywhere. I guess there's not really much of an alternative as it currently stands, but seeing how effective agentic AI is at chewing through data and analyzing systems makes me think that eventually, such systems will be used if they ever get to the necessary level of reliability.
That's not the same as saying that current architectures are acceptable, because clearly they aren't. But both neural net and stochastic controllers have been tested in aircraft since at least the 1990s. Probably earlier, but that's as far back as my knowledge goes, anyway. I don't know of any neural nets doing active control type tasks, but I don't see any intrinsic reason they couldn't be used as long as you can show that they're good enough.
Military experience, especially with unmanned systems, is largely irrelevant. They operate on a different set of rules and are generally willing to accept a higher level of risk in order to accomplish the mission.