Space
exploration will lead to space migration and eventually space
exodus. The lifespan of our planet is limited and dependent on the
life of the Sun. There have been approximate calculations made of
for how long would the Sun last before it burns all its
hydrogen. Yet, long before this will happen, the Earth will probably
be destroyed by some other natural cataclysm. As a most positive
effect, the freedom of expanding human society into space will allow the earth
to recover its natural glory. Present activities that pose a threat
to people and nature, such as hazardous industries, could be moved to
earth-orbiting stations and to the moon. A realistic artificial gravity could
be created by centripetal forces generated by spinning a space station on a
large radius circle.
Architectural Framework for a future
International Space Station 2
The
development of a space habitat is a long trial process that should include
extensive experimentation and testing of the various components. Following
is a proposal for an architectural framework for a pilot space station, with
the following objectives:
Creating
and Evaluating Artificial Gravity (AG)
Functional
Flexibility of components
Expandability
Experimental
Manufacturing in space
Economically
and technically feasible in the near future
The
main objective is to develop the infrastructure in space for evaluating the
long-term effects of Artificial Gravity on human health and functioning.
AG could be created through centripetal forces generated by spinning the living
quarters on a 50m radius circle. The revolving velocity will be one of
the parameters subject to experimentation.
The
ISS2 will be composed of 2 main assemblies. The Rotating Assembly (RAS)
will be revolving around an axle that is the centre of the Stem Modules
(SM). The Static Assembly (SAS) will remain fixed around the same
axle and will be connected to the RAS through the Motion Switch Hub (MS).
The MS will have a special core developed to allow communication between the
two assemblies without having to stop the RAS.
The
RAS will have 3 Space Habitat modules (SH). They will be kept in a stable
equilateral triangle configuration by 3 sets of Spoke Modules (SP), a central
Habitat Hub (HH) with Stem Modules (SM) and tension cables (C). Between
each SH and the peripheral SP, there will be a Propulsion for AG module (PA),
which will provide the forces for inducing and breaking rotation. The
Radius could be increased by adding SPs to the 3 spokes.
The
SAS will be used for Research and Manufacturing in Weightlessness, and will
provide the means to achieve the economic viability of ISS2, through joint
ventures with the private sector. The Manufacturing Modules (M) will form
hexagonal clusters of 6 units, attached to Manufacturing Hubs (MH) and
SMs. The Static Assembly (SAS) will also incorporate Docking Modules (D),
Fuel units (F) and Solar Arrays (S). The D, F and PD units at the end of
SAS can be moved by a Space Tug (ST) to allow the insertion of an HM and M
units, for expansion.
The
Central Command module (CC) will have its own D, F and Propulsion for Direction
(PD), and will be able to move from the top of the RAS to other docking
modules. The PDs will also control the positioning of ISS2. The SPs
and SMs will be cylindrical, with a central circulation tunnel and air locks at
both ends. The spoke and stem modules will have a circular cross section
with a core circular tube for circulation.
3STAR, a Pilot Space
Habitat
Several
designs for space habitats have been proposed in the last century, such as the
Stanford torus (1 mile diameter donut-shaped), the Bernal sphere (16 Km
diameter), the O'Neill cylinder (3 Km radius), and combinations of them.
In essence, they all create artificial gravity with centripetal force produced
by spinning the entire space station. Unfortunately, they have the disadvantage
of being very large and inflexible, in the sense that they could not serve
their purpose before being fully completed. This poses tremendous
economic and technological difficulties.
3STAR
is a relatively small-scale space prototype that could be technically and
economically feasible in the near future. Any earth-orbiting space
habitat could be developed in stages, using the present International Space
Station as a platform. This will make good use of the great achievements
of ISS and would ensure continuity in space exploration.
Having
the flexibility of conducting multi-disciplinary research is crucial for any
such prototype. 3STAR would provide independent modules for
facilitating parallel experiments in various scientific fields, permaculture,
energy self-sufficiency, simulated gravity, space architecture, low and
near-zero gravity manufacturing, etc. 3STAR provides this opportunity
thanks to its configuration that not only allows development in stages, but
also invites expansion.
In
the near future, 3STAR could provide a platform for travel to Mars and other
planets and for establishing a lunar base, avoiding Earth’s gravity. Its
telescope could observe the universe better than anything that could ever be
built on Earth. Furthermore, a next generation 3STAR could become
self-sufficient in time, able to break away from its earthly cradle and could
begin the human space odyssey.
There
is also tremendous potential for incorporating commercial components, which
would attract private investment and make the entire endeavor economically
viable. Tourism, lunar mining, production of rare metals and new
compounds, low-gravity manufacturing, are examples of activities that would
attract private enterprise.
3STAR,
as the name implies, resembles a three-pointed star forming an equilateral
triangle. This type of triangle is a “ground state” geometry providing
optimal stability and equilibrium. When completed, 3STAR would have three
geodesic spheres, one at each point, revolving in perfect balance in a circular
trajectory around the central hub, interconnected with cylindrical stems and
stabilized by an array of cables.
The
author has named the geodesic sphere BUCKYGLOBE, in memory of Richard
Buckminster Fuller, one of the greatest geniuses that ever lived. Due to
the large radius required, the stems (including spokes) will have intermediate
nodes and tension cables. As a result, the entire complex will resemble a
giant spider net.
The
illustrations indicate a circular trajectory with a diameter of 1000m, yet the
required minimum radius and velocity that the spheres will have to spin in
order to simulate a gravity sufficiently close to 1g (9.81
meters per second per second) will have to be calculated based on mathematical
formulas for centripetal force and acceleration, derived from Newton’s laws.
As
the mass of the components located near the centre of the complex, mainly the
Hub, will gradually increase with the addition of various building materials,
equipment, furnishing, etc., the rotation velocity can decrease, requiring less
energy.
If
an object is traveling in a circle with a varying speed, its acceleration can
be divided into two components, a radial acceleration (the centripetal
acceleration that changes the direction of the velocity) and a tangential
acceleration that changes the magnitude of the velocity.
Other
products of artificial gravity that affect human comfort also need to be
addressed; such are centripetal acceleration, head-to-foot gravity gradient,
angular velocity (max. 6 rotations per minute, but max. 2 for optimal comfort),
tangential velocity (minimum 6m, but ideally 10m per second), cross-coupled
head rotations and the Coriolis effects.
By
Newton's second law of motion, a physical force Fc must
be applied to a mass to produce this acceleration. The direction of the force
is inwards, towards the center of the circle and opposite to the direction of
the radius vector. If the applied force is less or more than Fc,
the object will "slip outwards" or "slip inwards", moving
on a larger or smaller circle, respectively.
Following
are quotations from "Artificial Gravity and the Architecture of Orbital
Habitats" by Theodore Hall, Proceedings of 1st International Symposium on
Space Tourism, Daimler-Chrysler Aerospace GmbH., 20 March 1997:
“…comfort
in artificial gravity depends as well on other aspects of environmental design,
beyond the basic rotational parameters…“Only the global centripetal
acceleration represents "design gravity". The other components are
gravitational distortions that arise from motion within the environment. They
affect the magnitude and direction of the total acceleration, causing changes
in the apparent weight of objects and the apparent slope of surfaces. Taking
Earth as the norm, one's experience of gravity should be independent of one's
motion. Hence, the goal is to design the environment such that the global
centripetal acceleration yields some preferred level of artificial gravity
while the other components. The equations suggest that the angular velocity
should be kept low and that the radius should be large.”
ECOSYSTEM
The
goal is to create an ecosystem that will gradually become self-reliant and
independent. The supply of all essentials, namely air, water, food
and energy, would gradually shift from being imported from Earth, to being
produced in the space habitat and reproduced in closed natural cycles.
At
the beginning, an artificial atmosphere will have to be created with Oxygen
brought from Earth. When the Moon will become a source of raw materials,
Oxygen can be extracted from lunar ice and other minerals, together with many
other elements used in manufacturing.
In
time, plant life shall generate most of the Oxygen required for maintaining a
high air quality. The amount of CO2, essential for plant growth, will
have to be monitored to maintain a healthy balance of gases in the air.
Water
can be a by-product of power cells that produce energy from burning Hydrogen
and will also be part of an artificially created natural cycle. Rain can
be produced from the condensation of water vapor in contact with the outer cold
surface of the Buckyglobe. For growing food, permaculture principles will
be applied.
Permaculture is
both a philosophy or lifestyle ethic as well as a design system that utilizes a
systems thinking approach to create sustainable human habitats by analyzing and
duplicating nature's patterns (ecology).
3STAR
will incorporate a vast energy system, collecting solar energy and converting
it back and forth between chemical, kinetic and electromagnetic forms, with
Hydrogen as the main storage agent. As a result, the energy system will
have a symbiotic relationship with the air, the water and food production.
3STAR
has five main functional elements: the BUCKYGLOBE, the HUB, the STEM, the
ROBCON and the WEB.
BUCKYGLOBE
Each
Buckyglobe will enclose an independent ecosystem. The
three-dimensional space structure, made of tubular elements, will support a
double layer (or skin) to protect the micro-atmosphere created inside.
The main function of the outer layer will be to provide a radiation shield with
retractable insulated panels, which will regulate the sunlight penetrating
through the transparent panels. Some of the geodesic segments could have
solar panels inserted; others incorporate adjustable shutters for regulating
and screening the entire spectrum of solar radiation.
The
inner layer will provide an air & vapor barrier. Depending on the
locations facing the various interior components, some portions will be
transparent to provide sunlight and visibility; others will be designed to
support artificial soil for farming, animal shelters, and other permaculture
buildings.
The
space between the two layers may be used to accommodate fuel cells, batteries,
oxygen and hydrogen storage and other equipment. Here, the temperature
will have to be maintained within limits acceptable to such equipment, not for
humans. Therefore, maintenance work in this space will require protective
suits and oxygen masks, but not necessarily space suits.
The
axis of the Buckyglobe will be developed into the Stem, with a Spoke in its
centre. The Stem accommodates all circulation (staircase and elevator), a
power train (or electromagnetic catapult) and various service conduits and
cables. It also has a docking module and thrust rockets at the end.
A
special computer will regulate the acceleration and deceleration required to
maintain a constant gravity level in the Buckyglobe.
The
neighboring Buckyglobes will be visible up in the sky. The Hub can
also be seen over the head. The overwhelming image of the Earth will be
present everywhere. This will be psychologically reassuring. The
Hub will appear like a second sun, radiating solar rays and contributing to
natural light.
The curvature resulting from the 500m revolution radius translates into a slope of 2.60%. To
simplify construction, the floor structure may be designed with straight
structural elements and creating stepped levels as required, introducing stairs
and ramps for communication between levels. The largest storey is 26m
wide; this would require a total stepping of approximately 675mm. If the
floor needs to be curved for improved comfort, this can be achieved with a
light concrete topping which can add thermal mass for energy efficiency.
The
architecture will be functional and pleasing and the building will be able to
grow like a tree, in phases. Resembling an evergreen tree, the stem/trunk
will support two stepped building blocks. Each building level will have a
slightly different gravity, which offers many opportunities, functionally and
for medical research.
The
dwellings and the various amenities, such as daycare, school, hotel with
restaurant, shops, medical clinic, fitness clubs, theatre, offices, etc., can
be located according to the most suitable gravity level. For example,
people with reduced mobility would probably prefer less gravity. On the
other hand, it would be unpleasant to have food jumping off your plate in the
restaurant, or feeling too light in the movie theatre.
This
space will receive artificial rain produced by condensation from the air/vapor
barrier. The interior skin around the “south” pole will be covered
with thicker soil and could be used for farming. The inevitable dust
created in the Buckyglobe will be deposited here due to centripetal force and
will turn into fertile soil. A small collection pond for storing water
could be created here as well and would become an essential component of the
ecosystem.
HUB
The
Hub is composed of two main bodies, resembling the mechanics of a
bicycle: The wheel is connected to the Buckyglobes (which would be part
of the tire) by the stems (spokes) and revolves around the fixed spindle,
through magnetic levitation.
The
two rings will be designed as a giant electromagnet (dynamo in a reversed
action). The Rotor is made up of many electromagnets placed in concentric
circles. The Stator would store batteries and other equipment. The
circulation between the revolving and the fixed bodies will be done in the
transfer rings, using moving escalators and walkways. An air seal ring will
prevent air from escaping into space.
The
Hub will incorporate a nuclear reactor, possibly of fusion type, after the
current research and experimentation would be completed, and would potentially
transmit energy to Earth through a technology that still remains to be
established (i.e. high-power waves, such as laser beams).
The
Hub will accommodate docking facilities and workshops where the components
received from Earth will be prepared for assembly in space by Robcons. Due to
its microgravity, the Hub can include highly robotized manufacturing of new
products and compounds that would be very difficult, or even impossible to
produce on Earth.
The
thrust to induce rotation will be provided by a system of booster engines (i.e.
ion rocket) mounted at the end of the stem. A second system will
fire outwards on the axis as needed to maintain the Buckyglobe at a constant
distance from the HUB before it is taken over by the centripetal force.
These engines will also act in case of emergency to maneuver the Buckyglobe and
stabilize its position vis-à-vis the HUB in case it would malfunction or the
tethering cables would fail.
In
an initial phase of development, before a connecting stem is constructed, the
Buckyglobe will be kept in balance on a spoke and tether cables system, that
would also incorporate power and communication conduits.
STEM
(SPOKE)
The
Stems accomplish several tasks. First, they support the Buckyglobes and
other space modules. Then, they connect the Buckyglobes to the Hub and
provide circulation throughout the entire system. The stems transmit the
spinning motion from the Hub’s Rotor to each Buckyglobe. Finally, they
incorporates mass drivers (or catapults), also called electromagnetic guns, for
projecting transportation shuttles and cargo shells into space.
In
the initial phases, before the Stems are constructed, Spokes will be needed to
provide a minimum compression capability for keeping the spheres at constant
distance from the Hub. This will be achieved with sections of pipe of approx.
1m diameter, sufficient to allow a construction crew to go through it.
The diameter and length of the sections will depend on the carrying capacity of
the lunching rockets or space shuttle which will bring the 3STAR components
into space. They could also be used to store other cargo during this
process.
Due
to the large distance between the Hub and the Buckyglobes, tension cables will
probably be required to prevent the Spokes from bending. These cables are
placed at critical nodal points on the Spoke and will be integrated in the
Web.
The
Stems shall have a built-in capacity for expansion, so that future modules can
be added. The cylindrical sections shall be designed to also carry cargo
from Earth the first time they are sent to the space station. They shall
also be designed to receive attachments for various services and future
expanded nodes. These will break down the Spokes into more manageable
travel segments and will shelter various amenities, utilities, storage and
manufacturing facilities.
For
flexibility and security, each Stem and Buckyglobe shall have its own station
for generating power and all basic elements such as oxygen, hydrogen &
nitrogen, all required for subsistence. This station shall be located
somewhere between the Hub and the geodetic sphere.
WEB
(SOLAR SAIL)
The
Web will be designed to have a multitude of roles. First, it ensures the
stability of the entire system, through tension cables acting like a spider
web. The cables will link the critical nodes located on the Hub, Stems
and Buckyglobes. This will be especially important before the Stems or
Spokes are completed, when booster rockets will achieve continuous tensioning.
Here
again we learn from nature; spider webs are among the strongest structures in
nature (if not the strongest), when we consider the strength they achieve per
unit of material used.
The
web could also support solar panels and could act as a Solar Sail that uses
radiation pressure. There is always the possibility that 3STAR will have
to be moved to another orbit around the Earth, or in the distant future to
another location in the solar system, or beyond. Then, the Solar Sail
will prove to be very useful.
Finally,
the web will support power and communication cables and a giant antenna for
deep space communication.
SPACE
CONSTRUCTOR
The
construction of the 3STAR would require the development of a versatile space
construction vehicle for installing the various components and for providing
transportation between the ISS and 3STAR before the Stems are in place.
After the interior links are established, its role would be limited to
transporting larger objects that exceed the capacity of the Stem elevators, and
of providing exterior maintenance and repairs.
This
space vehicle should be able to accommodate 2 workers in a protected
environment, and should have the minimum facilities required for work shifts
lasting several hours. It should have several robotic arms and have
extended visibility from its cabin, through a television camera system.
The
Space Constructor needs to be carefully planned to minimize the impact on the
Earth’s environment and the risk to erection crews. The entire vehicle
should be manufactured on Earth and be able to fit into a cargo ship or into a
cylindrical component of a lunching rocket.
ROBCON
The
geometry of the ROBCON (Robotic Constructor) consists of two main volumes: a
tetrahedron with truncated vertexes and a triangular prism, both with chamfered
edges. This shape creates maximum functional space and structural
integrity with minimum air volume and materials required (i.e. the largest
space is provided where needed, at the seats level). The tetrahedron
accommodates two communicating (but independent) Command Cabins with swivel
seats and large television screens for maximizing external views, separated by
an emergency sliding door.
Bumpers
mounted on the truncated vertexes of the tetrahedron, facilitate maneuvering by
preventing damage from potential collisions and three telescopic magnetic
landing legs ensure stability in any position.
The
Utility Cabin has several functions. It creates an access vestibule from
the Service Compartment, is used as a change room for space suits, and also has
a snack bar. But most importantly, it provides an emergency shelter
and has a dry toilet.
The
triangular prism encloses the Service Compartment, which is divided into three
chambers. The Air Lock provides pressurization and access through an exterior
hatch and a floor hatch into the Utility Cabin. Another chamber services
the manoeuvring thrust system. The third chamber accommodates the folding
robotic arms which, when not used, are tucked between the upper edges of the
triangular prism and the base of the tetrahedron.
The
control cabin can accommodate a crew of two. Below each row of
command seats there are two robotic arms that fold against the body of the
triangular prism in inactive position, so each worker can use two independent
arms.
The
core incorporates upper and lower manoeuvring thrust systems, which will
require very frequent starting and stopping. To eliminate a possible
failure of ignition, hypergolic propellants should be used (they spontaneously
burn when they are combined), such as liquid Hydrogen or Hydrazine combined
with Peroxide. Unsymmetrical Dimethylhydrazine [(CH3)2NNH2],
also known as UDMH, is another useful propellant. Another option is to
use cold gas propulsion.
Furthermore,
carriers may be attached on all three sides, for transporting various
components, such as geodetic struts and panels for constructing the Buckyglobe.
Following
the completion of Research, Design and Development, which will include
laboratory experimentation on a scale model, all components of 3STAR can be
manufactured simultaneously on Earth; then, they would be sent into space, and
assembled near the ISS.