If the SpaceX Starship ends up working as planned, it will do the same things our rockets do now, but at one one-hundredth the price. In an inspiring blog post, Casey Handmer argues that even people within the industry have yet to appreciate the qualitatively different opportunities that this price drop would enable:

By refilling in LEO, a fully loaded deep space Starship can transport >100 T of bulk cargo anywhere in the solar system, including the surface of the Moon or Mars, for <$100m per Starship. Starship is intended to be able to transport a million tonnes of cargo to the surface of Mars in just ten launch windows, in addition to serving other incidental destinations, such as maintaining the Starlink constellation or building a big base at the Lunar south pole.

Second, and more importantly, shoehorning Cassini 2.0 or Mars Direct into Starship fails to adequately exploit the capabilities of the launch system. Not to pick on Cassini or Mars Direct, but both of these missions were designed with inherent constraints that are not relevant to Starship. In fact, all space missions whether robotic or crewed, historical or planned, have been designed with constraints that are not relevant to Starship. 

What does this mean? Historically, mission/system design has been grievously afflicted by absurdly harsh mass constraints, since launch costs to LEO are as high as $10,000/kg and single launches cost hundreds of millions. This in turn affects schedule, cost structure, volume, material choices, labor, power, thermal, guidance/navigation/control, and every other aspect of the mission. Entire design languages and heuristics are reinforced, at the generational level, in service of avoiding negative consequences of excess mass. As a result, spacecraft built before Starship are a bit like steel weapons made before the industrial revolution. Enormously expensive as a result of embodying a lot of meticulous labor, but ultimately severely limited compared to post-industrial possibilities. 

Starship obliterates the mass constraint and every last vestige of cultural baggage that constraint has gouged into the minds of spacecraft designers. There are still constraints, as always, but their design consequences are, at present, completely unexplored. We need a team of economists to rederive the relative elasticities of various design choices and boil them down to a new set of design heuristics for space system production oriented towards maximizing volume of production.

As they say, read they whole thing, especially the part about space tractors. I leave you with one final quote:

It is time to raise the scope of our ambition and think much bigger