
Given the enormous start-up costs of the O'neill vision, it seems unlikely that
Island one will be the first colony to be built. I have been looking at a
different approach. My idea centres around placing a workshop in L5, that is
specifically designed to construct SPS modules. For lack of a better name, I
will call this island A. The basic element of the workshop is an iron sphere,
approximately 40 metres in diameter. The sphere rotates twice per minute. The
sphere is divided into cylindrical floors. The floors are divided into crew
quarters, manufacturing workshops, ore processing facilities, a hydroponics bay
and a satellite assembly hall. The satellite assembly hall is a cylinder that
lies along the axis of rotation. At each end of this assembly hall, there lies
an airlock. These are used both during the launch of finished SPS modules and
for the docking of supply ships, ore carrying ships and various other
spacecraft. The assembly hall is 10 metres in diameter and 40 metres long.
Lunar ores are delivered to the facility through its axial airlocks. The
ores are then taken to a small workshop, where they are processed into
manufacturing materials such as Calcium, Titanium, Iron, Aluminium, Magnesium,
Silicon, Rutile, Ilmenite, e.t.c. These materials are then used in various other
small workshops for the manufacture SPS parts.
The assembly hall is far too small to house a full scale SPS satellite. For
this reason it may be easier to produce the SPS in modules and assemble them
tele-robotically outside of the habitat. If a 20MWe SPS can be manufactured and
assembled in one week, then a 1000MWe SPS could be built in 1 year. If we assume
a 40 year life time, and a 0.1$/KWhr rate of return, the SPS will be produce
$35billion through out its life time. This amount would certainly exceed the
cost of producing it.
iron. Out of all lunar derived metals, iron is the easiest to produce. It is a
by-product of oxygen production. The entire facility could be formed by vacuum
deposition of iron, onto a thin shell of polymer. The Polymer shell would need
to be brought up from Earth, but would only weigh a few hundred kilos. The
interior cylindrical floors and assembly hall would be constructed in the
similar way. The oxygen that is liberated from the iron, will be useful when the
time comes for habitat pressurisation. The entire habitat might weigh in at
200-300 tonnes, minus the furnishings. Most of this mass will be lunar
materials.
The construction crew could be housed within a converted shuttle external
tank, during construction. This would be fitted out in LEO, and lifted to L5
using low thrust ion engines. The crew housing, would probably resemble a Zubrin
style Mars hab. The external tank could be shipped back to LEO and fitted out as
a ferry, after construction of the workshop is completed. A solar electric
propelled ferry, would be extremely useful for shipping people and materials
between low-Earth orbit and L5.
Despite its small size, island A will require a relatively large amount of
shielding. If we assume that 250g/cm2 of shielding (about 1/4 of what we get on
Earth) is an adequate amount, roughly 12,000 tonnes of shielding would be
required. A lunar mass driver, equipped with a 1Mwe nuclear power source, would
deliver this amount of shielding to L2 in about 1 year.
Tony
Learn how to build a profitable business
on the internet.
http://www.sixfigureincome.com/?854665

Rotation seems to me to be a nice-to-have rather than a minimal requirement
for an initial orbital workshop.
hollroa@...
Please respond to
ssi_list
Given the enormous start-up costs of the O'neill vision, it seems unlikely
that
Island one will be the first colony to be built. I have been looking at a
different approach. My idea centres around placing a workshop in L5, that
is
specifically designed to construct SPS modules. For lack of a better name,
I
will call this island A. The basic element of the workshop is an iron
sphere,
approximately 40 metres in diameter. The sphere rotates twice per minute.
The
sphere is divided into cylindrical floors. The floors are divided into crew
quarters, manufacturing workshops, ore processing facilities, a hydroponics
bay
and a satellite assembly hall. The satellite assembly hall is a cylinder
that
lies along the axis of rotation. At each end of this assembly hall, there
lies
an airlock. These are used both during the launch of finished SPS modules
and
for the docking of supply ships, ore carrying ships and various other
spacecraft. The assembly hall is 10 metres in diameter and 40 metres long.
Lunar ores are delivered to the facility through its axial airlocks.
The
ores are then taken to a small workshop, where they are processed into
manufacturing materials such as Calcium, Titanium, Iron, Aluminium,
Magnesium,
Silicon, Rutile, Ilmenite, e.t.c. These materials are then used in various
other
small workshops for the manufacture SPS parts.
The assembly hall is far too small to house a full scale SPS satellite.
For
this reason it may be easier to produce the SPS in modules and assemble
them
tele-robotically outside of the habitat. If a 20MWe SPS can be manufactured
and
assembled in one week, then a 1000MWe SPS could be built in 1 year. If we
assume
a 40 year life time, and a 0.1$/KWhr rate of return, the SPS will be
produce
$35billion through out its life time. This amount would certainly exceed
the
cost of producing it.
The facility itself could be produced almost entirely from lunar derived
iron. Out of all lunar derived metals, iron is the easiest to produce. It
is a
by-product of oxygen production. The entire facility could be formed by
vacuum
deposition of iron, onto a thin shell of polymer. The Polymer shell would
need
to be brought up from Earth, but would only weigh a few hundred kilos. The
interior cylindrical floors and assembly hall would be constructed in the
similar way. The oxygen that is liberated from the iron, will be useful
when the
time comes for habitat pressurisation. The entire habitat might weigh in at
200-300 tonnes, minus the furnishings. Most of this mass will be lunar
materials.
The construction crew could be housed within a converted shuttle
external
tank, during construction. This would be fitted out in LEO, and lifted to
L5
using low thrust ion engines. The crew housing, would probably resemble a
Zubrin
style Mars hab. The external tank could be shipped back to LEO and fitted
out as
a ferry, after construction of the workshop is completed. A solar electric
propelled ferry, would be extremely useful for shipping people and
materials
between low-Earth orbit and L5.
Despite its small size, island A will require a relatively large amount of
shielding. If we assume that 250g/cm2 of shielding (about 1/4 of what we
get on
Earth) is an adequate amount, roughly 12,000 tonnes of shielding would be
required. A lunar mass driver, equipped with a 1Mwe nuclear power source,
would
deliver this amount of shielding to L2 in about 1 year.
Tony

Rotation seems to me to be a nice-to-have rather than a minimal requirement
for an initial orbital workshop. Maybe, but if he's intending duty shifts of a year or more, some level of artificial gravity would be good. But with a rotation rate the same as Island 1, but with only a fraction of the diameter, I'm thinking the centrifugal force produced would be much less than a G. "How much is enough" is still an open question, but I suspect some gravity will be better than none. The kind of thing he's talking about is what they called the SpaceManufacturing Facility or SMF(or sometimes the "construction shack") back in the old studies.
Regards,

Valery Polyakov spent 437 days on Mir. So we have proof positive that a
duty stay of 437 days followed by return to Earth is acceptable. I
speculate that that could be stretched to a yet even longer period of time.
Let's suppose that a duty stay of two years is acceptable. How necessary
is rotation?
"Combs, Mike"
ssi_list@... ssi_list@...
04/20/01
09:02 AM
Please
respond to
ssi_list
Rotation seems to me to be a nice-to-have rather than a minimal
requirement
for an initial orbital workshop.
Maybe, but if he's intending duty shifts of a year or more, some level of
artificial gravity would be good.
But with a rotation rate the same as Island 1, but with only a fraction of
the diameter, I'm thinking the centrifugal force produced would be much
less than a G. "How much is enough" is still an open question, but I
suspect some gravity will be better than none.
The kind of thing he's talking about is what they called the Space
Manufacturing Facility or SMF (or sometimes the "construction shack") back
in the old studies.
Regards,
Mike Combs

>>>>Rotation seems to me to be a nice-to-have rather than a minimal requirement
for an initial orbital workshop.>>>>
a time, seems a bit dubious to me. When they get back to Earth and suddenly find
that their bones are brittle due to de-mineralisation, are we likely to get
sued? Just how necessary is gravity going to be, when it comes to casting
materials, or separating out suspended mixtures? At a rotation rate of 2 revs
(0.209rad/s) an equivalent of 0.09g's will be produced at a radius of 40m. Crew
quarters and some ore refining workshops that require gravity, should therefor
be placed on the bottom floor outer most floor) of the 'construction shack'. An
object sitting on the floor of the assembly hall will experience a pull of only
0.022g's. This should make the handling of fragile SPS components much easier.
I certainly do agree that eliminating rotation enormously simplifies the
problem of engineering a workshop. An initial workshop might be constructed from
two external tanks. This would be cramped and uncomfortable, but much easier to
set up. But in truth, I wonder about the wisdom of using external tanks. If we
can purchase one from NASA at a cost of $50 million or less, then it would be
worth while using them. If the cost of the tanks is much greater than that, then
it would be much easier and safer to simply launch a ready made space craft
using the Russian Energia. I have heard lift costs for Energia, quoted at around
$2500-$3000/Kg.
Tony
Learn how to build a profitable business
on the internet.
http://www.sixfigureincome.com/?854665

>>>Valery Polyakov spent 437 days on Mir. So we have proof positive that a
duty stay of 437 days followed by return to Earth is acceptable. I
speculate that that could be stretched to a yet even longer period of time.
Let's suppose that a duty stay of two years is acceptable. How necessary
is rotation?>>>
easier to design rotating machines rather than a rotating manufacturing
facility. The construction of the facility would be simpler if gravity were
eliminated.
Tony
Learn how to build a profitable business
on the internet.
http://www.sixfigureincome.com/?854665

The volume of a shuttle external tank is approximately 2000m2 or 68600 cubic
feet. Does anyone know what its exact dimensions are?
Learn how to build a profitable business
on the internet.
http://www.sixfigureincome.com/?854665

Rotating or non-rotating, it stretches imagination to believe that people
would continue to be productive beyond 437 days couped up inside a tin can
40 meters in diameter. If a 40-meter sphere is their entire world, then
probably psychological factors will dominate physiological factors once we
get above a year duty stay. We have to bring these people back down to
Earth so they don't go crazy. People are not robots.
anyway. If a person is not going to stay for years and years, then I
don't see why we have to design for rotation. We know already that people
can survive a 437-day stay in microgravity and return safely to Earth. We
really don't need to make an orbital workshop any more complicated than it
minimally needs to be.
As for use of rotation to separate out suspended particles in industrial
processes, these types of processes can be achieved with small-radius
rotating components. Fluids don't get dizzy like humans do when confronted
with small-radius simulated gravity. We don't need to rotate the entire
station to support specific industrial processes.
In a high-risk environment, both technically and financially, design for
what you minimally need. Minimalism.
Ron Menich
hollroa@...
Please respond to
ssi_list
>>>>Rotation seems to me to be a nice-to-have rather than a minimal
requirement
for an initial orbital workshop.>>>>
The idea of keeping a large number of workers in zero-g for months or
years at
a time, seems a bit dubious to me. When they get back to Earth and suddenly
find
that their bones are brittle due to de-mineralisation, are we likely to get
sued? Just how necessary is gravity going to be, when it comes to casting
materials, or separating out suspended mixtures? At a rotation rate of 2
revs
(0.209rad/s) an equivalent of 0.09g's will be produced at a radius of 40m.
Crew
quarters and some ore refining workshops that require gravity, should
therefor
be placed on the bottom floor outer most floor) of the 'construction
shack'. An
object sitting on the floor of the assembly hall will experience a pull of
only
0.022g's. This should make the handling of fragile SPS components much
easier.
I certainly do agree that eliminating rotation enormously simplifies the
problem of engineering a workshop. An initial workshop might be constructed
from
two external tanks. This would be cramped and uncomfortable, but much
easier to
set up. But in truth, I wonder about the wisdom of using external tanks. If
we
can purchase one from NASA at a cost of $50 million or less, then it would
be
worth while using them. If the cost of the tanks is much greater than that,
then
it would be much easier and safer to simply launch a ready made space craft
using the Russian Energia. I have heard lift costs for Energia, quoted at
around
$2500-$3000/Kg.
Tony

Given that, I wouldn't expect duty stays much longer than 437 days or so
anyway. If a person is not going to stay for years and years, then I
don't see why we have to design for rotation. We know already that people
can survive a 437-day stay in microgravity and return safely to Earth. We
really don't need to make an orbital workshop any more complicated than it
minimally needs to be. Then let's say that one might expect the initial SPS construction workersto work duty shifts from a year to 400 days duration and then get rotated back to Earth. Than at a later point, after accumulation of significant experience in space construction, we might expect a newer SMF with large, rotating crew quarters or perhaps even an Island 1 in order to reduce transportation costs by extending duty shifts to several years. Of course Island 1 offers the prospect of reducing "commuting costs" to essentially 0 by providing the option of having workers who live in space full time. But I think everyone's in agreement that Island 1 won't get built at the onset of the program, and even O'Neill agreed with this point.
Mike Combs
(903)-868-6314

>>>>Given that, I wouldn't expect duty stays much longer than 437 days or so
anyway. If a person is not going to stay for years and years, then I
don't see why we have to design for rotation. We know already that people
can survive a 437-day stay in microgravity and return safely to Earth. We
really don't need to make an orbital workshop any more complicated than it
minimally needs to be.>>>>
One tank would function as an assembly hall, with an airlock at one end, while
the other(s) would be divided into small ore processing facilities, component
manufacturing workshops and crew quarters. A big difficulty that I can see is
the shielding problem.
Using a spherical pressure vessel gives us a big advantage in that respect.
The surface area/volume ratio of a sphere is the smallest of any three
dimensional shape. We therefore require less shielding and the amount of refined
metal that is required to produce the pressure vessel, is kept to a minimum.
It might therefor be a better idea, to push the ET's up to L5, and simply use
them as a source of Aluminium for the construction of a spherical pressure
vessel. Burnt out rocket stages (like the upper stage of Ariane) might be useful
in this respect.

>>>>>Rotation seems to me to be a nice-to-have rather than a minimal
requirement
>for an initial orbital workshop.>>>>
>
> The idea of keeping a large number of workers in zero-g for months
or years at
>a time, seems a bit dubious to me. When they get back to Earth and
suddenly find
>that their bones are brittle due to de-mineralisation, are we likely
to get
>sued?
Couldn't be same thing be done by semi telerobotic operation with
only a common support structure and minimal sheilding. Every machine
and process used for the construction shack will be specially designed
so why not design for zero human presence?
Mitchell James
mejames@...
http://www.InnerTransit.net (Email distribution for multilevel organizations)
http://www.InnerTransit.org (Homebase for collaborative engineering)

There was a back of the envelope design by O'Neill shortly before his death.
It called for 6-8 Shuttle external tanks to be tethered together and spun
providing necessary volume for a small 100 person colony, workstation place.
SSI
> Rotation seems to me to be a nice-to-have rather than a minimal
requirement
> for an initial orbital workshop.
>
> Ron Menich
>
> hollroa@...
ssi_list@...
Island A
> Please respond to
> ssi_list
>
> Given the enormous start-up costs of the O'neill vision, it seems unlikely
> that
> Island one will be the first colony to be built. I have been looking at a
> different approach. My idea centres around placing a workshop in L5, that
> is
> specifically designed to construct SPS modules. For lack of a better name,
> I
> will call this island A. The basic element of the workshop is an iron
> sphere,
> approximately 40 metres in diameter. The sphere rotates twice per minute.
> The
> sphere is divided into cylindrical floors. The floors are divided into
crew
> quarters, manufacturing workshops, ore processing facilities, a
hydroponics
> bay
> and a satellite assembly hall. The satellite assembly hall is a cylinder
> that
> lies along the axis of rotation. At each end of this assembly hall, there
> lies
> an airlock. These are used both during the launch of finished SPS modules
> and
> for the docking of supply ships, ore carrying ships and various other
> spacecraft. The assembly hall is 10 metres in diameter and 40 metres long.
> Lunar ores are delivered to the facility through its axial airlocks.
> The
> ores are then taken to a small workshop, where they are processed into
> manufacturing materials such as Calcium, Titanium, Iron, Aluminium,
> Magnesium,
> Silicon, Rutile, Ilmenite, e.t.c. These materials are then used in various
> other
> small workshops for the manufacture SPS parts.
> The assembly hall is far too small to house a full scale SPS satellite.
> For
> this reason it may be easier to produce the SPS in modules and assemble
> them
> tele-robotically outside of the habitat. If a 20MWe SPS can be
manufactured
> and
> assembled in one week, then a 1000MWe SPS could be built in 1 year. If we
> assume
> a 40 year life time, and a 0.1$/KWhr rate of return, the SPS will be
> produce
> $35billion through out its life time. This amount would certainly exceed
> the
> cost of producing it.
>
> The facility itself could be produced almost entirely from lunar
derived
> iron. Out of all lunar derived metals, iron is the easiest to produce. It
> is a
> by-product of oxygen production. The entire facility could be formed by
> vacuum
> deposition of iron, onto a thin shell of polymer. The Polymer shell would
> need
> to be brought up from Earth, but would only weigh a few hundred kilos. The
> interior cylindrical floors and assembly hall would be constructed in the
> similar way. The oxygen that is liberated from the iron, will be useful
> when the
> time comes for habitat pressurisation. The entire habitat might weigh in
at

There would be much more architectural freedom to choose alternative
configurations of the tanks if they did not rotate. For example, seven
tanks could be arranged in hexagonal closest packing arrangement if that
were desired (just an example --- I don't know whether hexagonal closest
packing arrangement would be good or bad, but at least you'd be able to
consider it in a non-rotating design).
rotate. The inside of a tank is curved. Only certain orientations of
the tanks will allow efficient use of that space when there is gravity.
If the workshop doesn't rotate, then curved walls aren't that constraining.
Ron Menich
"Bettie
04/20/01
01:38 PM
Please
respond to
ssi_list
There was a back of the envelope design by O'Neill shortly before his
death.
It called for 6-8 Shuttle external tanks to be tethered together and spun
providing necessary volume for a small 100 person colony, workstation
place.
SSI
>
> Rotation seems to me to be a nice-to-have rather than a minimal
requirement
> for an initial orbital workshop.
>
> Ron Menich
>
> hollroa@...
ssi_list@...
Island A
> Please respond to
> ssi_list
>
> Given the enormous start-up costs of the O'neill vision, it seems
unlikely
> that
> Island one will be the first colony to be built. I have been looking at a
> different approach. My idea centres around placing a workshop in L5, that
> is
> specifically designed to construct SPS modules. For lack of a better
name,
> I
> will call this island A. The basic element of the workshop is an iron
> sphere,
> approximately 40 metres in diameter. The sphere rotates twice per minute.
> The
> sphere is divided into cylindrical floors. The floors are divided into
crew
> quarters, manufacturing workshops, ore processing facilities, a
hydroponics
> bay
> and a satellite assembly hall. The satellite assembly hall is a cylinder
> that
> lies along the axis of rotation. At each end of this assembly hall, there
> lies
> an airlock. These are used both during the launch of finished SPS modules
> and
> for the docking of supply ships, ore carrying ships and various other
> spacecraft. The assembly hall is 10 metres in diameter and 40 metres
long.
> Lunar ores are delivered to the facility through its axial airlocks.
> The
> ores are then taken to a small workshop, where they are processed into
> manufacturing materials such as Calcium, Titanium, Iron, Aluminium,
> Magnesium,
> Silicon, Rutile, Ilmenite, e.t.c. These materials are then used in
various
> other
> small workshops for the manufacture SPS parts.
> The assembly hall is far too small to house a full scale SPS
satellite.
> For
> this reason it may be easier to produce the SPS in modules and assemble
> them
> tele-robotically outside of the habitat. If a 20MWe SPS can be
manufactured
> and
> assembled in one week, then a 1000MWe SPS could be built in 1 year. If we
> assume
> a 40 year life time, and a 0.1$/KWhr rate of return, the SPS will be
> produce
> $35billion through out its life time. This amount would certainly exceed
> the
> cost of producing it.
>
> The facility itself could be produced almost entirely from lunar
derived
> iron. Out of all lunar derived metals, iron is the easiest to produce. It
> is a
> by-product of oxygen production. The entire facility could be formed by
> vacuum
> deposition of iron, onto a thin shell of polymer. The Polymer shell would
> need
> to be brought up from Earth, but would only weigh a few hundred kilos.
The
> interior cylindrical floors and assembly hall would be constructed in the
> similar way. The oxygen that is liberated from the iron, will be useful
> when the
> time comes for habitat pressurisation. The entire habitat might weigh in
at
> 200-300 tonnes, minus the furnishings. Most of this mass will be lunar
> materials.
>
> The construction crew could be housed within a converted shuttle
> external
> tank, during construction. This would be fitted out in LEO, and lifted to
> L5
> using low thrust ion engines. The crew housing, would probably resemble a
> Zubrin
> style Mars hab. The external tank could be shipped back to LEO and fitted
> out as
> a ferry, after construction of the workshop is completed. A solar
electric
> propelled ferry, would be extremely useful for shipping people and
> materials
> between low-Earth orbit and L5.
>
> Despite its small size, island A will require a relatively large amount
of

I concur with the need to design for significant teleoperation. Whether
humans could be entirely absent from an orbital workshop is an open issue.
I suspect that for any significantly complicated thing that we wish to do
in the near future, humans will be required to some extent. Should the
orbital workshop be continuously crewed, or should it be occasionally
human-tended when there is a need to do especially complicated tasks.
Unknown.
Mitchell James
ssi_list@...
04/20/01 10:29
AM
Please respond
to ssi_list
>>>>>Rotation seems to me to be a nice-to-have rather than a minimal
requirement
>for an initial orbital workshop.>>>>
>
> The idea of keeping a large number of workers in zero-g for months
or years at
>a time, seems a bit dubious to me. When they get back to Earth and
suddenly find
>that their bones are brittle due to de-mineralisation, are we likely
to get
>sued?
Why the assumption that workers are required for this operation?
Couldn't be same thing be done by semi telerobotic operation with
only a common support structure and minimal sheilding. Every machine
and process used for the construction shack will be specially designed
so why not design for zero human presence?
Mitchell James
mejames@...
http://www.InnerTransit.net (Email distribution for multilevel
organizations)
http://www.InnerTransit.org (Homebase for collaborative engineering)

>>>There would be much more architectural freedom to choose alternative
configurations of the tanks if they did not rotate. For example, seven
tanks could be arranged in hexagonal closest packing arrangement if that
were desired (just an example --- I don't know whether hexagonal closest
packing arrangement would be good or bad, but at least you'd be able to
consider it in a non-rotating design).>>>
is we could mould the tank material into a sphere. External tanks are long, thin
cylinders. This is a wasteful way of producing a pressure vessel. If you want to
maximise internal volume, you need a sphere.
An easy way to do this is to cut the ET's up and vacuum deposit the aluminium,
onto a thin (0.1mm) kevlar sphere. The biggest single advantage associated with
using a spherical facility, is the minimisation of a great deal of shielding
material. This is going to weigh thousands of tonnes in any event.
Tony
Learn how to build a profitable business
on the internet.
http://www.sixfigureincome.com/?854665

>>>>Why the assumption that workers are required for this operation?
Couldn't be same thing be done by semi telerobotic operation with
only a common support structure and minimal sheilding. Every machine
and process used for the construction shack will be specially designed
so why not design for zero human presence?>>>>
plan. But, I am rather dubious of the practicality of the entirely automated and
tele-controlled manufacture of such complex systems. The fact is that
manufacturing can be a fiddely job, that occasionally requires a pair of human
hands. Machines can have a nasty habit of screwing up. They get dirty and
require cleaning. The brushes in the motors degrade and require replacing. The
thing that I don't like about the idea of an entirely robotics system, is the
fact that it has little adaptability, there is no 'bend' in it. The robots
certainly can reduce the requirement of human presence, but can they eliminate
it entirely? It is worth investigating, but personally I have my doubts.
Non the less, reducing the required man power to a minimum, will be important
in the first space facilities. It will reduce the cost of maintaining the
facility. The psychological pressures within the facility will also be less.
There are two key methods to reducing psychological stress in a confined space.
One, is to keep the astronauts mind busy and active. This will assure that
he/she will not die of boredom. Another, is keeping plenty of greenery within
the habitat.
Tony
Learn how to build a profitable business
on the internet.
http://www.sixfigureincome.com/?854665

There would be much more architectural freedom to choose alternative
configurations of the tanks if they did not rotate. For example, seven
tanks could be arranged in hexagonal closest packing arrangement if that
were desired (just an example --- I don't know whether hexagonal closest
packing arrangement would be good or bad, but at least you'd be able to
consider it in a non-rotating design). It's funny you should use this as an example. I remember one of the space manufacturing reports which included a paper on a SMF design which used a rotating baton shape with 7 clustered tanks at each end, with each tank pointing "upward". Each tank was split into 7 levels, each of which was divided into 3 pie-shaped wedges. So each tank in both clusters could provide 21 apartments. Interior space planning would be less constrained if the workshop did not
rotate. The inside of a tank is curved. Only certain orientations of
the tanks will allow efficient use of that space when there is gravity.
If the workshop doesn't rotate, then curved walls aren't that constraining. I've always felt that there would be lots of wasted space inside the kind of tank stations advocated by the Space Islands group, where they're trying to join the tanks end-to-end to form a torus. (Or at least one would have to choose between wasted spaceor decks which were not level in most locations.) In the baton type approach I mentioned, where the tanks are vertical instead of horizontal, I think there would be less wasted space, even with concentric-arc shaped decking.
Mike Combs

In a message dated 04/20/2001 6:34:26 AM Pacific Daylight Time,
rmenich@... writes:
Date: 04/20/2001 6:34:26 AM Pacific Daylight Time
Reply-to: ssi_list@...
Valery Polyakov spent 437 days on Mir. So we have proof positive that a
duty stay of 437 days followed by return to Earth is acceptable. I
Note that Dr. Polyakov is a medical physician who took a lot of care to keep
himself in good shape. He spent several hours a day excrcising, and was not
available to do much in the way of other duties.
Consequently, upon his return to Earth he was walking unaided on his first
day back Earthside.
Other cosmonauts who spent less time in space, but did a lot less excercise,
were in much poorer shape and could not walk for a couple of days.
A regime where workers must spend more than half their waking hours
excercising gives very little time for actual work, so their productivity
will be quite low.

>>>Consequently, upon his return to Earth he was walking unaided on his first
day back Earthside.
were in much poorer shape and could not walk for a couple of days.
A regime where workers must spend more than half their waking hours
exercising gives very little time for actual work, so their productivity
will be quite low.>>>
Assuming that we were to rotate our station at a rate of 2 revs, the gravity
created at a distance of 20m from the axis of rotation, would be only 0.8773
N/Kg or 8.9% (1/11th) Earth normal. This may have some advantages when it comes
to manufacturing, but it is unlikely to be much help when it comes to
maintaining Human health. The average man would weigh only 6.5 kilos.
Tony
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Over the weekend, I made some rough calculations for the pressure vessel that we
would need, for the outer hull of Island A. I assumed an Iron pressure vessel.
This would be constructed from lunar Ilmenite derived Iron, that was processed
in a small initial facility, within a shuttle external tank. Depending upon how
the Iron is treated, a wide range of material properties are possible. So I
assumed that we would be dealing with a soft, pure iron, purified using the
Carbonyl process. In this case, the tensile strength of the soft iron would be
about 500MN/m2, and its properties would closely resemble those of mild steel. I
assumed a safety factor of 8. This probably is not excessive, given that the
pressure vessel is all that stands between the crew and oblivion. I also assumed
that the facility would be pressurised to 1/2 atm. The thin walled pressure
vessel equation, yields a wall thickness of 0.8cm. Given that the density of
pure iron is 7900Kg/m3, and the radius of our pressure vessel is 20m, the mass
of the vessel comes out to be 317.677 tonnes. In order to produce this much
Iron, we would need to reduce 862 tonnes of Ilmenite, into Fe, TiO2 and O2. The
pressure vessel itself could be formed using vacuum deposition, so the initial
external tank facility would only need to reduce and purify the the iron. This
could be achieved by hitting lunar Mare soil, with hot carbon monoxide and
passing the resulting vapour through a fractionating column. The pure iron
carbonyl, will condense out at its own specific temperature. It could then be
decomposed into carbon monoxide and pure iron. The depleted lunar soil residue
from the process, can be used as a shielding material.
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>>>A submarine is a small self contained little world where
people are constantly in each other face and would not have much more
room than a SMF is likely to have. Just like an SMF you can't step
outside to get away from it all for a little while. ( granted the SMF
crew could go for a spacewalk ) In thinking about lengths of stays you
have to remember that the people who crew an SMF will be there primarily
to build things, they will not be astronauts in the original sense of
the word . They will not be doing research.>>>
long as possible. The manufacturing company would offer financial incentives to
those who are prepared to tolerate longer stays. Careful design of the SMF,
would ensure that each crew member had some private space that he/she can
disappear off to, when they need to get away from their colleagues. Separate bed
chambers are probably a must, for long stays. It is also quite likely that
plants would be included within the habitat. The thing that astronauts on MIR
missed the most, were green living things. The presence of plants would help
keep the atmosphere clean and reduce the amount of carbon that needs to dumped
over the side. Fresh fruit and vegetables would also help to prevent scurvy and
malnutrition, and would have a notable effect on crew morale. Plants could be
brought up as seeds or saplings. In short, the presence of plants on a space
voyage, will have a very positive effect upon crew morale, psychology, physical
health, and the smell and CO2 content of the air. Even a crowded workshop would
have a plant in the corner. Hall ways and recreational rooms would be full of
them. Private spaces could be sectioned off using green plants. Although space
is likely to be scarce in an SMF, it should be noted that SMF's do not have to
be designed for battle conditions. For an SMF at L5, or in orbit around a NEA,
duty stays of 2-3 years may be necessary. Under these conditions, privacy,
greenery and recreation will be essential for those wishing to remain sane.
Tony

I can see that we are talking at partly crossed purposes here. The SMF I
am considering would be in Earth Orbit, be it high or low and be used as
a stepping stone to building bigger facilities. The one that you are
talking about appears to me to be a somewhat ideal one that could be
sent out on a voyage to the asteroids ( wherever they are ) in which
case yes there would have to be long stays. For the type I am talking
about fresh fruit and Vegetables would be brought up on the supply
vessels. As for financial incentives I imagine that any initial job will
be highly paid no matter how long you are up there for. Green Plants
would be nice, but in a zero G ( or almost ) environment does anyone
know what will happen to them ? I know there have been experiments on
germinating seeds, but larger plants ? ( I realise that that is a
separate discussion in itself ) Also separate quarters / bed chambers
would be nice but impractical at the beginning. Of course once the
facility is running they could expend some time on expanding the
facility so that it could incorporate these things. The first facilities
are likely to be Rough and Ready. In other words quickly built with a
minimum of comforts, just enough to get the work done with minimum
expense. They will be cramped, smelly, crowded and most likely partly
dangerous and most definitely ugly, but they will get the job done. Not
everyone will want to or be able to work in those conditions but they
will pave the way for bigger and better facilities. If we try and go
for the better facilities straight away all we will be doing is
hampering ourselves.( both mentally and financially )
before , and that is the spreading of skills and experience. If you are
up there with a small number of people for a long time, they will gain
the experience but not be able to pass it on to many people. On the
other hand if you have a large number of people who are rotating
through, your skills base will be much larger. Some of these people will
leave your company for whatever reason and go on to work for another
company and pass on this experience to them and so on. A large base of
people here on earth with the desired skills and experience ( no matter
who they work for ) would have to make colonising space easier than a
small number of people with those skills.

I found an on-line illustration of the ET station configuration I was trying to describe below. This is from Al Globus' website. http://lifesci3.arc.nasa.gov/SpaceSettlement/spaceres/images/figII2-1.GIF
Mike Combs
There would be much more architectural freedom to choose alternative
configurations of the tanks if they did not rotate. For example, seven
tanks could be arranged in hexagonal closest packing arrangement if that
were desired (just an example --- I don't know whether hexagonal closest
packing arrangement would be good or bad, but at least you'd be able to
consider it in a non-rotating design). It's funny you should use this as an example. I remember one of the space manufacturing reports which included a paper on a SMF design which used a rotating baton shape with 7 clustered tanks at each end, with each tank pointing "upward". Each tank was split into 7 levels, each of which was divided into 3 pie-shaped wedges. So each tank in both clusters could provide 21 apartments. Interior space planning would be less constrained if the workshop did not
rotate. The inside of a tank is curved. Only certain orientations of
the tanks will allow efficient use of that space when there is gravity.
If the workshop doesn't rotate, then curved walls aren't that constraining. I've always felt that there would be lots of wasted space inside the kind of tank stations advocated by the Space Islands group, where they're trying to join the tanks end-to-end to form a torus. (Or at least one would have to choose between wasted spaceor decks which were not level in most locations.) In the baton type approach I mentioned, where the tanks are vertical instead of horizontal, I think there would be less wasted space, even with concentric-arc shaped decking.
Regards,
Mike Combs

Thanks for the reference. Kind of makes one want to cry. In 14 tanks
could live 252 people comfortably; so says the site you reference. In 100+
Shuttle flights so far, our government has not seen fit to deliver even one
external tank to orbit. Potential orbital housing for over 1500 people
sits at the bottom of the Atlantic. We're currently $4 billion over
budget on a Space Station that at max would house only a handful or two of
people. And NASA says that Tito needs an armed guard to go pee in the
middle of the night while he's on it, despite joy rides it gave to Jake
Garn, John Glenn, and others on the Shuttle in years past.
preaching to the choir.
Ron Menich
"Combs, Mike"
ssi_list@... ssi_list@...
04/27/01
08:56 AM
Please
respond to
ssi_list
I found an on-line illustration of the ET station configuration I was
trying to describe below. This is from Al Globus' website.
http://lifesci3.arc.nasa.gov/SpaceSettlement/spaceres/images/figII2-1.GIF
Regards,
Mike Combs
There would be much more architectural freedom to choose alternative
configurations of the tanks if they did not rotate. For example, seven
tanks could be arranged in hexagonal closest packing arrangement if that
were desired (just an example --- I don't know whether hexagonal closest
packing arrangement would be good or bad, but at least you'd be able to
consider it in a non-rotating design).
It's funny you should use this as an example. I remember one of the space
manufacturing reports which included a paper on a SMF design which used a
rotating baton shape with 7 clustered tanks at each end, with each tank
pointing "upward". Each tank was split into 7 levels, each of which was
divided into 3 pie-shaped wedges. So each tank in both clusters could
provide 21 apartments.
Interior space planning would be less constrained if the workshop did not
rotate. The inside of a tank is curved. Only certain orientations of
the tanks will allow efficient use of that space when there is gravity.
If the workshop doesn't rotate, then curved walls aren't that
constraining.
I've always felt that there would be lots of wasted space inside the kind
of tank stations advocated by the Space Islands group, where they're
trying to join the tanks end-to-end to form a torus. (Or at least one
would have to choose between wasted space or decks which were not level in
most locations.) In the baton type approach I mentioned, where the tanks
are vertical instead of horizontal, I think there would be less wasted
space, even with concentric-arc shaped decking.
Regards,
Mike Combs
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Looks like they have done some major renovations to the site since the
last time I looked at it. Much better now than it used to be.
B