On 21 June 2014 13:37, 'Chris de Morsella' via Everything List <
[email protected]> wrote:

>  *From:* LizR <[email protected]>
> *To:* [email protected]
> *Sent:* Friday, June 20, 2014 6:10 PM
>
> *Subject:* Re: Solar power's "bright future"
>
> >>That raptor rocket surely doesn't have *much* higher delta V than, say,
> the Saturn 5? No chemical reaction is going to be that much more efficient,
> no matter that you turn it into a superheated flying bomb. Surely for human
> exploration beyond the Moon you really need (a) a moon base, (b) and
> orbital assembly plant supplied from the moon base, and (c) some form of
> nuclei/ion propulsion for your long haul space craft (which also need
> shielding, of course!)
>
> I agree -- nothing I have heard about really improves on the chemical
> potential of H2(liquid)/LOX. The advantage of LNG is not that it is pound
> for pound a better fuel/oxidizer combo than liquid hydrogen/LOX (Saturn 5),
> because it isn't, but rather because LNG fuel allows for significantly
> longer longevity of the rocket fuel tanks and rocket motors components
> themselves. Hydrogen causes metals to become brittle; whereas LNG does not
> (or does not to the degree that hydrogen does). On a long duration mission
> -- say to Mars and back -- it becomes rather important that the rocket
> engine components do not wear out prematurely. That would be a real bummer,
> for the unlucky astronauts.
>
> The innovative aspects of the Raptor engine are not just in terms of the
> type of fuel it uses, but also because it uses separate turbo injection for
> the LNG and LOX using floating bearing (essentially the spinning parts of
> the turbo pump actually are floating on a very thin film of the LOX or LNG.
> This also very significantly improves rocket engine life (those bearings
> wear out fast). And by (apparently) choosing to use separate turbo pumps
> for the LNG and the LOX it removes a catastrophic failure point for designs
> that employ a single turbo pump with a diaphragm separating the LOX from
> the fuel (whatever it is) -- if the diaphragm fails in such a design it is
> an almost guaranteed catastrophic failure.
>
> Again I agree -- if we are ever going to become a space fairing
> civilization we need to learn to live off the land (the land up there). The
> moon has a very much smaller gravity well than planet earth; it just seems
> to me to make sense to get the mass of fuel and LOX at the very least and
> perhaps other materials as well from there (or from NEO asteroids as well)
>

Yeah, having a long lasting booster isn't much use if you can only fire it
for a few hours. (Antimatter wears out your rocket even faster than
hydrogen, but it sure gets you there a lot quicker!)

>
> >>Or use chemical propellant to rendezvous with one of those asteroids I
> mentioned, then sit back and wait out the 9 months or so to Mars.
> (Preferably installing a permanent base in the asteroid, which effectively
> becomes a mars shuttle.)
>
> The asteroid Eros 433  would seem to fit the bill for a transit station.
> It is fairly big (the second largest NEO in fact); it is an Amor type
> asteroid and is a Mars crosser.
>

It comes within something like 20 million miles of Earth, I think, so yes a
distinct possible. (And it isn't an alien space ship, as it turned out to
be in a story I wrote when I was about 12. Oh well, predicting things is
hard, especially the future.)

>
> >>I wish I could type this without my hands shaking with excitement. We're
> actually trying to go to Mars!!!!!!
>
> I really hope so :)
> Chris
>
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