Hmm, NASA, the President, and the international partners are all willing to commit to the biggest Multibody option to launch the core, initial piece of Freedom, without which none of the rest can work, at a time when even the M02 has not been launched nor yet a single prototype even been built for ground static testing?
Here--I guess it might be a mix of things. Part of it is Vulkan panic, part might be a very great confidence that what Boeing draws on paper is sure to fly flawlessly when fleshed out.
Well, recall that Multibody's core is basically just a stretched Saturn 1C--and Saturn 1C's flown a good 20 flights by 1982. So they're willing to trust Boeing that the core will work, which just leaves the question of will the clustering work. Boosters are nothing new, the only difference here is that the boosters and core are roughly identical, so that's also not seen as hugely risky if they trust the basic core--which again is basically just a stretched Saturn 1C. There's more technical details to support those gut feelings, but to be really simplistic, it doesn't feel as risky as relying on a wholly new LV probably should.
I'm sure that the funding must include a few test flights, first of M02, then of solid-boosted versions, finally an all-up H03.
We'll get into the testing and such in a later post, but...yeah, there will be some demo flights.
The only cargo I can envision for the H03, assuming there are no gung-ho plans on the table yet for grandiose manned ventures beyond LEO, would be launching Freedom's core.
The core, and the inner two truss segments. Reread the update. And given how critical those components are, and the fact that R&D and construction costs on them will probably exceed a billion $, adding a couple hundred million to fly a risk-reduction Heavy starts to seem like a good deal.
For that matter, while you do tell us that HSM masses pretty much the full LEO capability of H03,
I have to go look that up
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Wow, 70 tonnes! I guess there's capacity for a big fairing after all.
Forgot how big Multibody is, didn't you.

It's okay, happens to me sometimes.
So--would manned versions of the basic craft still be considered a subtype of "Minotaur," or would that evolution merit a whole new name?
We'll see when we get there, but strategicially Minotaur as a stepping-stone to a manned vehicle has a lot in common with the SpaceX Dragon (though the designs are pretty different in the technical details, they're both leveraging a cargo need as an excuse for developing and testing the critical components of a manned system). I'd be inclined
What, every single time? Why?
It's not like the Service Module or solar panels are coming down in the capsule and being reused.
No, but they're not NASA and don't have NASA's budget, so they're looking harder for ways to save a bit. If refurbishment doesn't work out, they'll just fly them expendably, like NASA's Apollos, but they think it's worth investigating. As for why recover at all, building a separate variant without TPS would cost a fair bit, and somewhat defeat the secondary role of demonstrating for future manned operations, while Minotaur's downmass actually provides a pretty useful capability on its own--in fact, it's perhaps more important than its upmass. Samples, entire experiment racks, station hardware (small stuff, like life support sumps or computer components)...there's a lot that's interesting to have back if something's already headed downhill, and not a lot of room in an Apollo descent module once you account for the crew. NASA doesn't really need maximum upmass from ESA's craft, but having a good 3.5 tons of downmass on every flight is appreciated a lot--again, look at the SpaceX Dragon. On theflight next week, SpaceX-1 is manifested to only carry 500 kg to the station, but it's manifested to carry almost triple that
down.