Re: Regolith eating raptors
The Blue complaint had something about raptors tearing up the regolith, putting bits of it in orbit and those bits coming back and hitting Starships or astronauts. That was a valid complaint about the earliest concepts. The current plan is that the raptors shut down before the Starship gets too close to the moon and the final descent it handled hot gas thrusters firing diagonally from above the tanks. The return trip starts with thrusters and switches to raptors when high enough. The top of the tanks is high up on current Starships and expected to be even higher on HLS so there will be enough propellant to go from LEO to the Moon and back to NRHO with a full load of propellant.
The little legs on current Starships are a temporary solution. HLS Starships will have big legs and wide feet. There are cargo missions planned with other landers that will reach the Moon before Starship. One of these could survey a proposed landing site.
The long drop from the crew habitats to the surface is a valid concern. Starship has lots of mass margin so there is room for multiple redundant solutions. The good news is that NASA cannot use Starship's full return cargo capacity. They can only bring back what will fit between the astronauts in an Orion capsule.
Congress requires NASA astronauts to go to the moon in an Orion capsule launched on an SLS rocket and return to Earth in that capsule. This places other limits on the missions: Only one mission per year as that is the maximum rate SLS can be manufactured. SLS can only get Orion to NRHO. Before NASA had a ride to the moon there was a plan to put a space station (LOP-G) there so that Orion+SLS would have somewhere to go. The 2024 deadline means that LOP-G will not be there in time.
NRHO is not that far from low lunar orbit. The propellant for the return portion of that trip is not that bad either. Bringing that propellant from the surface of the Moon to LLO requires lots more propellant. Bringing lots of propellent from LLO to the moon requires a huge amount of propellant. Dynetics almost solved this with a clever design with extra propellant tanks that get dropped shortly before landing. Blue solved this by breaking the LOP-G to the moon and back ride into three parts that get delivered to NHRO separately and assembled by crew at LOP-G (and disassembled on the moon!). SpaceX solved it with a really big Starship. Just imagine crew getting out of their cramped Orion into a small LOP-G and living there until it is time to leave for the moon in a huge luxury Starship bigger than the ISS.
Once Starship has done its return trip to the Moon there is then the question of what to do with it. Going to an Earth-centred elliptical orbit is quite cheap. Aerobraking to LEO in one go melts HLS starship. Getting there with multiple small aerobrakes means that the electronics get fried in one of the many trips through the radiation belts. Burning propellant to get to LEO requires a large amount of propellant. It is hard to match orbits in an elliptical orbit so a tanker cannot sensibly meet a returning starship there, but a tanker could go to NRHO, deliver enough propellant for a round trip to the Moon and get back to Earth with its heat shield and flaps. HLS Starship has an endurance of only 100 days so it cannot wait for another Orion. NASA will hire another starship. If only there were some other human rated ride to NRHO.
Servicing HLS Starships for multiple trips is tricky. Time to build Moon Base Alpha.
The balance of a crew/cargo/tanker Starship returning to Earth is a problem. Without doing something clever most of the mass is at the base. The lower flaps would have to be huge and stick right out. The upper flaps would have to be small and mostly folded up leaving little margin to control descent. The solution is to put the small tanks for landing propellant high up in the vehicle. The small oxygen tank goes right at the top.