> Anyway, getting back on topic. Maybe the US should sell a couple of
> Shuttles and the hardware jigs to Japan, who seem to be making a lot of
> noises about getting to the iss recently.

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A clever person solves a problem.
A wise person avoids it. -- Einstein
>It's becoming obvious that Ares I is a real dog and that a "man rated" EELV
>would be faster, better, cheaper, and safer.
I think you'll find that the Delta IV is already effectively 'man rated'
anyway - compared to the shuttle and certainly compared to the Ares1 - it's
a smoother ride, is already proven and, in my opinion, safer as it doesn't
us a solid main stage.
Have a look at the Soyuz - it's size and mass let it fit inside the payload
fairing of the Delta IV Medium - capable of over 8 tonnes into LEO. Rather
than designing the Orion, maybe they should design an Americanised Soyuz.
If the mass of the orbital module were combined with that of the re-entry
module, you'd easily get six crew spaces. It would basically be as if the
Soyuz Service Module were combined with a bi-conical CM.
bob haller safety advocate - 16 Aug 2008 00:09 GMT
> >It's becoming obvious that Ares I is a real dog and that a "man rated" EELV
> >would be faster, better, cheaper, and safer.
[quoted text clipped - 10 lines]
> module, you'd easily get six crew spaces. �It would basically be as if the
> Soyuz Service Module were combined with a bi-conical CM.
you really dont need to carry 6 people, aers was upsized to make it
impossible to use a existing expendable of any type.
it may cost a bit more but were better off launching more often, with
fewer people....
as shuttle taught us the cost is mostly infrastructure, the marginal
cost for more flights isnt that great
Jeff Findley - 18 Aug 2008 13:47 GMT
>>It's becoming obvious that Ares I is a real dog and that a "man rated"
>>EELV would be faster, better, cheaper, and safer.
[quoted text clipped - 11 lines]
> basically be as if the Soyuz Service Module were combined with a
> bi-conical CM.
A US clone of Soyuz isn't a great idea. For starters, I don't like the fact
that the orbital module and descent module are separate modules. More
complexity, more separation events, more things to go wrong.
The Apollo CM design isn't a bad one for a capsule. You get a lot more lift
than the Soyuz design, which means it's easier to get lower G's during
reentry, especially when you're coming back from the moon at much higher
velocities than you do with a LEO reentry.
Jeff

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A clever person solves a problem.
A wise person avoids it. -- Einstein