Not very efficient or reliable ones. Newcomen’s ‘atmospheric engine’ was basically an ad hoc design that could only produce up to about 5 hp and because of the poor understanding of the effects of thermal differences on the thermodynamic cycle, operated at extremely low throughput efficiency. Watt’s innovation of the jet condenser reduced pressure and thermal losses by separating the injection of the condensed working fluid from the main piston chamber, but was still monumentally inefficient and not possible of being scaled beyond about a 10 hp output. While some of the limitations were due to material strength and manufacturing tolerances, these engines were just terribly inefficient and were far to massive to be used for anything but stationary applications that required a constant low power supply (mostly used as water pumps for mines and canal locks). The way in which they fundamentally worked and how to gain the possible efficiencies were a mystery to Newcomen, Watt, and their contemporaries; the phase transition from liquid to steam and the resulting work that could be done was just so much magic. It required the development of the model of the Carnot cycle and investigation into the behavior of steam under various pressure conditions to really understand how a steam engine works and how to extract good efficiency for a given thermal gradient such that steam engines for practical mobile applications such as marine vessels or industrial high pressure applications could be built.
Well, sort of. We have a clear understanding of the elements of the necessary technology, but the specific experience and engineering details of how we did it are either lost or obsoleted by change of materials, processes, et cetera. We could not literally “go to the Moon today” because we don’t even have a launch vehicle currently capable of lifting sufficient mass to carry a human crew and lander to Lunar orbit. That we could build such a system is not in question, but constructed to modern engineering standards and processes would likely take just as long as the original Apollo program. Actually, most estimates of a timeline are much longer, but those also assume the extensive bureaucracy involved with getting NASA to approve of anything; practically speaking from a purely technical standpoint, we could probably design, develop, and qualify a new crewed Lunar-capable launch vehicle, spacecraft, and lander in [POST=17178323]no less than five years and more likely close to eight years[/POST] given an essentially blank check budget.
There will be, of course, those who argue that because we’ve done it before and have the “blueprints”, we could just rebuild the Apollo/Saturn system and do it again. Those people, however, will conveniently ignore that even setting aside the marginality of the Apollo spacecraft and Saturn V rocket compared to modern reliability and functionality standards, that there is considerable ‘tribal knowledge’ in any complex system to make it function, and simply aping what people have done in nominal operation in the past without going through the exercise of understanding how the system works (and how to determine when it isn’t working) is fundamentally cargo cult engineering. I work in this world every day, and there is no substitute for making your own mistakes and knowing not just the how, but the why of system function.
Stranger