At NASAspaceflight I was so baffled by the present Artemis HLS architecture (SLS + Orion + Lunar Starship) I suggested an alternate, more logical architecture preserving the statu quo, since Congress holds NASA purse and is self-obsessed with SD-HLV (= SLS) since 2010.
I suggested (half jokingly, TBH) to use SLS as a backup methalox tanker for LEO Starships, bound for Moon or Mars. Since they will need 4 to 14 tanking flights per BLEO mission; and since SLS at 70 mt to 130 mt has payload comparable to BFR-Starship.
The bottom line: so you created that goddam SLS at insane expense, over 12 years ?
But the flight manifest only has 5 Artemis moonshots until 2030 ?
Needs more flights to build more SLS and thus drop costs through larger production run ?
Well, now I have a crapton of SLS flight opportunities: backup methalox tanker flights for Starship bounds to Moon or Mars.
What I discovered is that SLS has a production & flight rate of two per year, at a cost of $2.5 billion a launch.
This mean that production and flight rates can't even been ramped up to 4, 6, or 8 flight per year even if some kind of "silver bullet payloads" were magically found. For example, the LC-39 launch pad (now single: SpaceX loaned the other) can't sustain higher flight rates.
Even throwing shitloads of billions of dollars at NASA, Artemis or SLS couldn't change that.
End result: flight a lot
or fly few
or fly none - SLS remains a very bad deal whatever happens.
Another alternate use of SLS would be: fly Mars Direct, you dummy. From 1991 to 2011 all it lacked was a SD-HLV. Now the said SD-HLV exists, called SLS.
And yet nobody is thinking to use if to make Mars Direct happens... at least !
In passing, that SLS-vs-Starship race reminds me of that novel...
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We are presently leaving through a ripoff of it. I mean: really.