Re: DIY space transport
- From: "Len" <len@xxxxxxxxxxxxxx>
- Date: 24 Jul 2005 11:19:48 -0700
Charles Buckley wrote:
> George William Herbert wrote:
> > Pete Lynn <pete@xxxxxxxxxxxxxxxxxx> wrote:
> >
> >>Even this seems to assume an inflexible pre-furnished module approach,
> >>not a bare shell approach that one then moves furnishings into. Kind of
> >>like buying a fully furnished caravan and then trying to attach it as
> >>one unit onto the side of a house, instead of buying a shell of a room
> >>and then adding light weight furnishings to taste.
> >
> >
> > The issue here is that the shell, structure, and hatches are
> > a small fraction of the total weight. Most of the weight is
> > systems and payload.
> >
>
> On the other side of that is the issue that most of the volume
> in the modules is air. Not shell, structure, hatches, systems,
> and payload. I seem to recall that volume constraints tend to
> drive launch vehicle choice as much as mass issues.
>
....snip....
I agree that size--almost as much as mass--has been an important
driver for launch vehcile design. That is, up to recently.
With our later concepts such as Space Van 2008, Space Van 2009,
and Windjammer 2010, size has been much less a driver. This is
due to our recent emphasis on very low wing loading ascent, as
well as reentry. This leads to relatively large vehicles that
are less sensitive to payload dimensions. I feel that this is
one of the main advantages of the very low wing loading approach.
Best regards,
Len (Cormier)
PanAero, Inc.
x@xxxxxxxxxxxxxx (change x to len)
http://www.tour2space.com
.
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- Re: DIY space transport
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