James E. D. Cline
Independent Researcher
9800-D Topanga Cyn Blvd #118, Chatsworth, CA 91311
E-mail: jedcline@earthlink.net http://home.earthlink.net/~jedcline/
Copyright © 1997 by James Edward David Cline. Published by the Space Studies Institute, Inc. with permission
Abstract
Similar to the dynamic braking of an electric motor/generator,
which connects the kinetic energy of the rotating armature into
a torque force drag against the stationary stator part of the
motor/generator, the electromagnetic drag of a rapidly rising
series of armature sections drags upward on the stationary part
of a very tall structure to exactly balance the weight of the
stationary structure, the lift force distributed along the structure.
With appropriately fast rising mass and electromagnetic coupling
balancing the distributed weight, earth surface to space transportation
structures become conceivable. The fast rising armature mass stream
also distributes electromagnetic lift drag energy coupling to
vehicles rising up that structure to space. Stabilized by laterally-coupling
mass stream pairs and by active position feedback servo systems,
these would

be dynamic transportation bridging structures. Seed KESTS would
be launched and flown up and around the planet back to the starting
point, then bootstrapped up to full working size. Such electrically
powered rail bridging transportation structures from Earth surface
to GEO could conceivably provide the massive transportation capacity
to build a new civilization encircling the Earth in the Clark
Belt geosynchronous orbit, a long term project hopefully to unite
humanity toward common cooperative venture goals.
A Brief Description of the KESTS Concept
Kinetic energy can stiffen and strengthen structures. Analogous
examples include balloons and pressurized fuel tanks that are
strengthened by the kinetic energy of the internal pressurized
gass omnidirectional kinetic energy; and a jet of high pressure
liquid creates an arch shaped structure in agravitational field.
The arch formed by that high pressure mass stream jet of liquid
could support the weight of a lightweight sheath around it, a
sheath unmoving relative to the ground, forming a kind of bridge
supported by kinetic energy.
Now consider an electromechanical analog of that high pressure
jet of liquid. Recall that electrical energy is converted to kinetic
energy by electrical motors, rotary and linear. Motors can be
designed to do the reverse, too, becoming an electrical generator
driven by kinetic energy. And torque or thrust is also coupled
between the relatively moving parts of a motor/generator.
Imagine an electric rotary motor/generator whose armature (rotor),
instead of spinning around a central shaft, slides around inside
the stator on a maglev (magnetic levitation) track. And imagine
that armature being in sections, not physically directly connected
to each other, like many trains riding the same maglev tracks,
in a circle.
Stretch out the motor/generator so big that it circles the Earth,
using the gravitational field to pull it around in a closed loop
which contacts the earthsurface on one part and then reaches out
to GEO far above the opposite side of the planet as it goes around.
Have the armature sections travel on the maglev tracks inside
evacuated tubing at above orbital velocity. Let the dynamic drag
of the upward-bound armature sections provide a lift force on
the track-stator-tubing exactly that amount required to support
the distributed weight of the tubing, making the tubing earthsurface-stationary.
This acts to compress the trajectory of the mass stream toward
the Earth. Thus the tensile strength of the tubing need only be
enough to cope with the static and live loads between drag lift
mechanism points along the tubing. As the creation of this lift
force extracts some of the kinetic energy from the armature mass
stream, each armature sections position and velocity is re-initialized
at the earthsurface contact site, initially drawing the energy
needed to do this from the earthsurface electrical power grid.
Continuing with this envisioning, put maglev tracks also on the
outside of the tubing, for payload-carrying vehicles to use. Enable
those vehicles also to drag electromagnetically on the high velocity
rising mass stream of armature sections, lifting the vehicles
up the structure from earthsurface to space, up to the GEO Clarke
Belt orbital altitude. Call this transportation structure a KESTS,
short for Kinetic Energy Supported Electrically Powered Transportation
Structures. Use the KESTS to lift construction materials up to
GEO for building the first few large-scale space habitats, such
as mile-diameter wheel-like habitats with 1-g STP interiors for
10,000 people each, including agriculture and light industry.
Build more of these large space habitats, mostly made of lunar
and asteroidal-sourced materials, loosely coupling them together
to infill the Clarke Belt with them. Each complete ring of them
is home for 15 billion people. Build enough KESTS to lift 1,000,000
people a day to the Clarke Belt Orbital Habitat Ring, along with
their household belongings. Make the Orbital Habitat Ring (OHR)
sufficiently safe and luxurious to entice the majority of the
earthsurface population to move up the KESTS to live in it, creating
a new primary site for human civilization. Restore the earthsurface
ecosystem to natural balance. Expand human civilization outward
from the Earths OHR. This is an outline of a KESTS to OHR (Kinetic
Energy Supported Electrically Powered Transportation Structure
to an Orbiting Habitat Ring) project.1
Purpose
Building transportation structures, a form of elevator-bridges,
to connect the ground all the way up to orbital altitudes may
seem absurd; however, such structures are being considered here.
The intent is to create a transportation system adequate to the
task of lifting the majority of the Earths population up into
space, lifting perhaps 7 billion people and their household goods
over a 20 year time span, to live in a ring of loosely coupled
large scale 1-g STP interior habitats encircling the Earth in
the geosynchronous Clarke Belt orbit. This is hoped will enable
a near-future vigorous expansion of earthlife into space, expanding
human civilization far beyond that possible in a closed ecosystem,
and restoration of the Earths surface ecosystem to a healthy
long term balance as a precious biological resource for the future.
An electrically powered bridging rail transportation structure
spanning between the earth surface and Geosynchronous Earth Orbit
seems most likely to have the capacity to be able to do that task.
Background
Historically, the urge to climb high to a safe haven may reach
as far back as the trees; in the dawn of civilization, the Tower
of Babel at E-Temen-An-Ki had the goal of building a tower from
ground to the heavens; in 1960 Artsutanov proposed a geosynchronous
centrifugally supported tether type of tower structure for supporting
an electric elevator into space; in 1982 Keith Lofstrom proposed
a kinetically augmented structure called a Launch Loop which was
a continuous belt loosely driven between two pulleys, the centrifugal
force of the loose belt flinging it to the fringes of the atmosphere
in its journey around the pulleys; in 1985 Rod Hyde proposed a
vertical tower enclosing a fountain of electromagnetically coupled
beryllium disks, which he calculated could lift the combined weight
of every human being on the planet up to the fringes of the atmosphere
while using only the electrical energy used by the City of Los
Angeles in a mere two weeks; and also in 1985 Earle Smith proposed
a continuous belt eccentrically reaching around the planet, contacting
the planetary surface on the equator and reaching geosynchronous
earth orbit at its high point above the far side of the planet.2,3,4,5,6
Quickly moving the primary site of human civilization off-planet
has been considered essentially an impossible option up until
now. But at the present time, human civilization piles up unrecyclable
toxic refuse, entropically dispersing metallic ore deposits beyond
reconcentration, burns the oxygen producing rainforests along
with their genetic treasures, and burns fossil fuels a million
times faster than a forested ecosystem could replace it. In terms
of population size, we long ago passed the limits for long term
sustainable levels for living in harmony with the natural ecosystem,
even given a fully aware and responsible humanity of only 10%
of the present population.
KESTS as a Key to an Overall Solution
People prefer to live in man-made structures, and space habitats
are about as man-made as you can get. So let us consider creating
a transportation system adequate to move some 7 billion people
over a period of 20 years out to the Clarke Belt, along with their
household belongings, plants and pets, along with all the agricultural,
industrial, and markets civilization needs for a solid resettlement
there. For now, let us just create the option; later humanity
can choose to utilize it or not. KESTS may be able to shoulder
that task, along with lifting the construction materials for the
first few such 10,000-person space habitats, solar electric power
stations, and construction materials for a head start in building
an asteroidal and lunar mining and materials processing base to
provide structural materials for most of the vast ring of space
habitats to orbit the Earth, a site for a great civilization and
way station to the solar systems resources there awaiting to
be brought to life.
Basic KESTS Technology
The compressive strength of known materials is very inadequate
to the task of bearing the weight of such immense structures,
so the compressive load would largely be carried by compression
of the trajectory of mass streams circulating within the structure
at above orbital velocities, the distributed weight of the fixed
structure supported by electromagnetic drag against the rapidly
rising armature mass streams. The mass stream armature sections
velocity are referenced to the Earth surface, so the load of the
weight of the structure, and payload moving in vehicles upon it,
is transferred by the mass streams to the ground load bearing.
The pulsing electromagnetic energy of magnets contained within
the armature mass stream is inductively coupled to the distributed
load of the structure, and to the vehicles traveling upon the
structure. Similarly, energy is put into the structure by electromagnetic
coupling to the mass stream at the earthsurface contact sites.7
To support the enormous weight of such earth surface to space
bridging structures, electrodynamic coupling of equally enormous
upward bound armature mass streams traveling within them circulating
at faster than orbital velocity, drag electromagnetically upward
on the earthsurface-stationary part of the structures, slowing
the upward bound mass stream slightly in return for support of
that weight, compressing the trajectories slightly toward the
Earth. This distributes the energy required to provide the upward
force that opposes the force of gravity on the earth-stationary
part of the transportation structure, electromagnetically dragging
against the structure as it rises, just enough to balance the
weight of the structure everywhere along its length, and supplying
a small position bias tension.
KESTS Analogy to an Electric Motor/Generator
The structure thus resembles an electric motor/ generator in an
electrodynamic braking mode, the mass of the motionless stator
being torqued by the electromagnetically coupled drag force from
the armature rotor whizzing past the stator, positioned such that
the torque provides an upward-oriented force opposing the force
of gravity. In this view the armature is the mass stream. and
the stator is the earthsurface-stationary part of the structure.

The Mass Stream Armature Sections
The mass stream is composed of armature sections performing several
functions. Their primary function is to provide the storage and
exchange of the kinetic energy which supports the compression
load of the structures weight, and distributes energy to move
payload along the structures. Some modified armature sections
may also function directly as vehicles transporting payload within
the mass stream itself, and other forms of armature sections may
be the payload itself on a one-way trip up or down as raw material.
Armature sections need to be designed to resist contact with each
other somehow avoiding such contact wear;

so perhaps they will need periodic automatic inspection and repair/replacement.
Armature sections exchange energy within the KESTS by rising/falling
in a gravitational field, and electrically through permanent and
induced magnetism, and electrostatically. The electric field energy
exchanges support the structure, center the mass stream within
the tubing, input and extract energy to the mass stream, sense
armature section position and velocity, for re-initialization
processes, and prevent physical abrasive contact.
KESTS Analogy to a Lasso
To picture how this structure fits into the gravitational space
around the Earth, lets mentally picture a cowboy's lasso, a circle
of rope spinning above his head, as in the following drawing.
Its semicircular shape is held by energy stored in the lasso,
by the centrifugal force distributed outward from the rope loop's
center of rotation.
Now mentally extend that fast-spinning rope so as to encircle
the earth, grazing the surface of the planet and also reaching
far out into space on the other side of the planet. Then sheath
the lasso in tubing to exclude air from the path in which it directly
moves, supporting the weight of the tubing by compressing it smoothly
along the radius of rotation of the spinning lasso, whose centrifugal
force would press back outward against the sheath. Attach this
tubing to the earth surface where the lasso grazes the planetary
surface: the tubing now is effectively a structure extending from
the ground out into space. Tapping some of the nearby speedy lasso's
kinetic energy, vehicles can lift up along the structure from
the ground into space, carrying no propulsion fuel aboard them,
like tram cars lifted into space.

The lasso rope is equivalent to the rotor in the motor analogy
(which is turn is analogous to the high velocity armature mass
stream), and the rim is equivalent to its stator (which in turn
is analogous to the earthsurface-stationary part of the structure).
Where the lasso/rotor is upward bound in the gravitational field,
it provides a lift force on the rim/stator. Laterally-coupled
counterrotating pairs of these structures provide upward-bound
lasso/rotor (mass stream) kinetic energy to provide lift force
to the rim/stator (earthsurface-stationary part of structure)
all along its length.
Each of the armature mass streams effectively travel on maglev
tracks inside tubing which forms the earthsurface-stationary part
of the KESTS structure, the rim/stator part of the structure in
the above analogy. On the outside of this earthsurface-stationary
tubing, payload-carrying vehicles travel along other maglev tracks.
They, too, electrodynamically brake against the rising mass stream
as they lift up from the surface of the Earth to the earth geosynchronous
orbital altitude, extracting energy from the rising mass stream
to provide lift force for the vehicles; this energy is intrinsically
distributed all along the transportation structure. Eliminating
need for electrical superconductors all along the structure for
transferring electrical power to raise vehicles along the structure,
the high velocity mass streams provide the energy to the point
of need everywhere along the structure, both to support the structure
against the force of gravity and to provide lift energy to vehicles
riding up to space along the structure.8

Vehicles descending from GEO to the earthsurface along the structure
electrodynamically brake against the earthsurface stationary part
of the structure. From the preceding diagram, you will see that
this is a force lifting the structure up away from the earth,
adding potential energy back into the structure.
Vehicles rising along the KESTS will drag the KESTS slightly downward
toward the planet in reaction, absorbing energy from the KESTS
mass stream in the process of lifting payload; and later when
descending back to the planetary surface, the vehicle electromagnetically
drags against the tracks of the KESTS, pulling upward on the KESTS
in the process of slowing its decent and thus restoring energy
back to the transportation system. Similarly, the counter rotating
laterally coupled pairs of mass streams, forced into matching
trajectories, conserve the overall energy

within the mass streams even though they continually are being
accelerated by each other away from their orbital paths. The efficiency
of this process will be determined by the various electrical to
kinetic energy conversion processes, especially the electromagnetic
bearing efficiency.
Earth rotates, so attaching the structure to the equator means
that the whole structure must similarly rotate too. A pair of
mass streams following a parallel course, but rotating in opposite
directions, and restrained to a common adjacent parallel trajectory
by lateral shear force coupling all along its length, forces the
mass streams to follow the rotation of the planet.
The electrical power input to the mass stream pairs initially
would be at the planetary surface contact sites, which also provides
the re-referencing of the mass stream velocities relative the
the ground. This electrical power would initially come from conventional
electric power grids, but then would convert over to space solar-electric
power sources. KESTS to GEO makes it easy to lift the weight of
construction materials for SSPS to GEO, which then would beam
millimeter wave energy back down to rectennas near the KESTS ground
site, providing power for the KESTS transportation structure.
Building more SSPS thusly in GEO would provide salable electric
power to the rest of the world, similar to what was originally
envisioned in the 1970's, although in that scenario SSPS construction
required a major lunar infrastructure first to provide construction
materials. An alternate power source form would be to attach solar-electric
power plant thrusters to the KESTS in space, which support their
non-orbital velocity weight component by thrust against the downward-going
mass streams, adding kinetic energy thusly to the mass stream,
which effectively lifts up on the laterally coupled upward-bound
mass streams, adding energy to the KESTS; excess mass stream kinetic
energy can be extracted by dynamic drag against the magnetically
pulsating downward-headed mass streams at the surface contact
sites, providing salable space solar-derived electric power to
commercial electric power grids as a byproduct, without requiring
microwave power transmission from space to the ground.
KESTS potentially have some interesting properties, primarily
useful as supportive structures for rail transportation between
the earth surface and earth orbital altitudes, as a distributor
of transportation energy along itself, as an energy storage system,
and possibly as a prime provider of solar-derived electric power
to earthsurface commercial electric power grids.
Electric elevator type access from ground to space has long been
of interest, because of its potential high efficiency, electrical
power source, low environmental pollution, and huge payload capacity,
as compared to chemical reaction engine propulsion transportation
systems serving in the ground-to-space function.
KESTS Dynamics
The dynamics which can be envisioned at this time for this form
of KESTS involve the coupling of the mass stream to its environment.
In some ways resembling the spinning rotor of an electric motor,
the mass of this armature is going around faster than the orbital
velocity at any altitude, held lower by the weight of the sustained
loads of passive structure and its live loads. The armature mass
stream couples to its environment through electrical fields. Pushing
from the earthsurface contact anchor re-initialization site, the
mass stream is re-accelerated and repositioned to restore energy
consumed along the KESTS pathway, compensating for live loads
and lateral forces on the KESTS. From this re-initialization site,
the mass stream heads back upward, electromagnetically dragging
weakly against the passive structure around its path, as well
as dragging against coupling to vehicles tapping that energy to
lift them up the KESTS. The passive structure involves the evacuated
tubing in which it flows, the shear coupling between counter rotating
stream tubes, and the guidance tracks for live loads such as passenger
vehicles. Note that live loads being lifted along the KESTS exert
a downward force on the structure's mass stream, but live loads
which are decelerating back toward the earth surface exert an
upward force on the tracks thus adding energy back into the transportation
system.
Non-uniform electromagnetic fields couple kinetic energy between
a circulating loop of high velocity mass, which appear as pulsating
magnetic fields to stationary parts of the mass stream's environment,
inducing alternating currents and defining the phasing for inputting
electrical power into the mass stream. The mass stream whirling
around a planetary body in an eccentric path, which contacts the
surface at its low point, is squeezed toward the planet by the
weight of portions of the structure which are stationary relative
to the planet.
Each mass stream is contained within the tubing in which it flows,
tubing which excludes the atmosphere where near the earth, supports
vehicular tracks, defines the path of the mass streams, and provides
structure for the lateral shear coupling between counter rotating
mass streams. Payload is carried primarily in vehicles on low-friction
maglev tracks, and the vehicles electromagnetically drag on the
upward-bound mass stream when rising up the KESTS.

KESTS to GEO, otherwise known as the Clarke Belt, would have the
advantage of requiring minimum difficulty embarking and disembarking
at either terminal due to velocities being intrinsically matched
at both ends, potentially a walk-on at earthsurface ground level,and
walk-off into the Clarke Belt easy process.4,7

KESTS to an Orbital Habitat Ring in Low Earth Orbit would reduce
the need for shielding of the habitats, and the KESTS would be
a significantly smaller structure. However, there would be a major
difference in velocity between the KESTS, which only rotates at
the angular velocity of the earth, and the Low Earth Orbit habitats,
so this form of KESTS would need to support a section of electromagnetic
rail accelerator structure, for providing the 18,000 mph delta
v between the KESTS and the Orbital Habitat Ring in Low Earth
Orbit.
KESTS Quasi-Elliptical Shape
The shape of the KESTS is only approximately elliptical. The armature
mass streams experience external forces all along their length,
not only from the orbital mechanics component of movement in the
planetary gravitational field, but also from the trajectory compression
distributed electromagnetic drag against the tubing weight support
sites, geometric electromagnetic mass stream benders, solar-electric
powerplant mass thruster sites, and vehicular live loads, all
of which act to distort the KESTS shape from a true ellipse.
Electromagnetic Mass Stream Benders
To give the mass stream re-initialization site a somewhat steeper
angle above the horizon to work with, electromagnetic mass stream
benders may be useful. Gravity gradient oriented, and position
held by modulating drag against both upware bound and downward
bound armature mass streams, benders would put a kink into the
shape of the mass stream passing through it, raising the launch
angle slightly.
KESTS Stabilizing Mechanisms
Stability of KESTS structures basically would come from a balance
between the slight upward stretch energy bias between the mass
stream and the weight of the stationary portions of the structure,
the overall structure being slightly stretched mechanically, taken
up by conventional tensile strength of materials of the tubing
and lateral coupling. Yet a KESTS would also be an active structure,
which can have its shape and lateral position adjusted by altering
the exit velocity vector of the mass streams at the ground contact
re-initialization site. Position stability would thus also be
controlled by anticipation of changing loads along the structure,
so as to resist wind loads and unbalanced vehicular loads around
the structure's length. All the differential expected loads need
to be integrated into the re-initialization launch vectors of
the mass stream as it exits the ground site, and the tubing and
lateral shear coupling portions of the structure need to be strong
enough to withstand these forces. If it is found that dynamic
anticipatory position feedback servoing is inadequate to adequately
stabilize the KESTS position, then passive dampers would need
to be installed along the KESTS.
Stresses in KESTS Tubing
The stresses on the solid part of the structure, which involves
the KESTS tubing structures, include the tensile load consisting
of the weight of the small section of tubing, lateral shear coupling
structure, maglev tracks on the inside and outside of the tubing,
and live loads riding outside the tubing, as summed over the distance
between electromagnetic drag mechanism sites on the tubing. These
sites are of necessity very close to each other, perhaps built
as an intrinsically distributed mechanism everywhere in the tubing.
Since electromagnetic drag against the rising high velocity mass
stream is adjusted to almost exactly match the weight of the solid
structure and live loads summed between drag mechanism sites on
the solid structure, the tubing does not carry significant amounts
of the weight of the rest of the structure, with longitudinal
forces thus very small in the tubing.
The wall thickness of the tubing will be defined mostly by the
above mentioned associated parameters of KESTS equations for a
particular manifestation of a KESTS structure. It would be a primary
parameter, of course, if the earthsurface-stationary tubing were
supported only by its hanging on the mass stream, thus requiring
a constant stress tubing crossection and requiring the strength
of perhaps diamond fiber. Such a more efficient KESTS perhaps
will evolve and be built when massive space manufacturing facilities
are available in the relatively distant future; but the present
concept is for KESTS structures which can be built from existing
materials without requiring significant advances in strength of
available materials, constructible and sustainable in the relatively
near future with only technology development required. Once the
OHR is established, undoubtedly technology advances will enable
the emplacement of new forms of large scale KESTS built in zero-g
high vacuum manufacture.
Emplacement of KESTS Around the Planet
Emplacing these extraordinarily large bridging structures represents
further engineering challenge. Bootstrapping processes seem appropriate,
building upon seed KESTS. Some KESTS seed emplacement techniques
include those which either launch & fly a single orbit back to
the launch site trailing seed KESTS tubing, propelled by reaction
thrust of expendable mass stream components being reversed in
direction in the nose piece, and providing temporary distributed
electromagnetic drag bending resistance to the trailing tubing;
or a rather brute force technique of launch of the mass stream
itself punching through the atmosphere driven by one of several
propulsion techniques (chemical reaction engines; mass drivers
of various types; or millimeter wave energy beams) upon which
then the initial tubing is laid. Such seed KESTS launch emplacements
surely will be a marvel of engineering and coordination and courage.
The initial seed KESTS could be emplaced from the re-initiallization
site simultaneously launched in opposite directions from the equator,
propelled by an expendable mass stream bouncing off the nosepiece
of the rising KESTS, perhaps initially assisted by high velocity
gas against its portions where leaving the ground, and/or by millimeter
wave directed beam energy inputting power distributed to the already
airborne portions of the KESTS to be used to then heat air as
reaction mass to provide upward thrust distributed along its length.
The nosepiece of the seed KESTS would be flown like an airplane
which is airborne high yet with portions still on the ground,
and flown around the planet, trailing the seed KESTS tubing, to
again return to the launch site from the opposite direction; the
lateral shear coupling then being added up both directions starting
immediately when both seed KESTS arrive at the re-initialization
site. Once the seed KESTS is thusly emplaced, it would be used
to support the lifting of ever larger KESTS tubing structures
upon it, bootstrapping until exponentially built to full capacity
size.
Early Emplacement Concepts
The techniques by Loftstrom and Smith involve laying the loop
mechanism on Earth surface across at least one ocean, then accelerating
the loop mechanism until it rises, or by carrying the upper portion
of the loop aloft with balloons prior to acceleration. Hyde's
vertical form of KESTS would be built by inserting new evacuated
sections at the Earth surface launch point, incrementally raising
the upper reflector end as sections are added at its surface base.
2,3,4
KESTS Emplacement by Flying Nose-Reaction Propulsion
The thrust of a mass stream against a structure which produces
a sudden 180 degree turn around of the mass steam, much as Rod
Hydes Starbridge fountain structure would have done, suggests
another emplacement means. Making the tube diameter a small fraction
of an inch and of flexible tubing would enable a small ground
construction site and expendable R&D launches. A large circular
mass driver would accelerate the mass stream up to, say, 20,000
mph while flowing within evacuated tubing which is configured
as a large coil. At the start of the launch the weight of the
nose

thruster, which provides the 180 degree turnaround of the mass
stream within itself, needs to be much less than the force of
the mass stream slamming against it to be electromagnetically
thrown backward by the nose thruster. Headed upward, the nose
thruster would resemble a conventional reaction engine launch,
if the version merely releases the mass stream into the environment
once it has expended its push against the nose thruster; more
advanced versions would provide laterally-coupled return tubing
for the reversed returning mass stream packets. The weight of
the rising mass of the uncoiling tubing would be supported by
distributed electromagnetic drag against the mass stream hurtling
through it, as in the conventional KESTS form. The nose thrusters
trajectory would arch over and down to the site of the other end
of the KESTS arch. Experience with building ever-longer arches
would increase until the arch has completely circled the planet
to have its landing site be at its launch site, thus emplacing
a seed KESTS into space, for bootstrapping construction of full
capacity structures. Nose thruster KESTS emplacement technology
offers seed-bootstrapping KESTS, temporary KESTS, and special
one-way materials delivery systems. A half-arch from ground to
GEO conceivably could provide one-way delivery of construction
materials; for example, if the mass stream is glass fiber with
magnetic inclusions in it, delivered at, say, 4 miles worth per
second, accumulates respectably.9
Chemical Reaction Engine Technology Emplacement
Another, rather brute force, emplacement method would use chemical
reaction engine technology to initially accelerate an upward bucket
chain of objects that form the energy storage mechanism that will
eventually support the KESTS. This technique establishes a parallel
contrarotating pair of tubeless KESTS mass streams first, then
installs evacuated tubing around it, forming the basic structure
of the KESTS. 10
Emplacement as a Millimeter Microwave-Boosted Launched Mass Stream
Similar to launch by the blast of chemically powered reaction
engine exhaust against it, multiple beamed millimeter wave energy
sources perhaps could utilize hot air plasma acceleration technology
to emplace seed KESTS. 11
KESTS to GEO But Not Anchored on the Equator
There may be possible KESTS configurations which attach to the
ground at sites mirrored about the equatorial plane, for example
attached at both New England and Argentina, or eastern China and
western Australia, instead of connecting at the equator itself.

Such KESTS structures would have more convenient transportation
terminal sites for existing centers of civilization, and even
be a means for transporting between those distant ground sites
by way of space; although they would have different stabilization
parameters and require perhaps double the construction materials
to build than would equatorial KESTS.
Comparison with Tether Types of Transportation
KESTS perhaps will eventually be supplanted by centrifugally-supported
equatorial tethers, for long-term sustenance transportation between
Earth surface and near-space. Indeed, KESTS might well provide
the immense payload lift capacity to GEO useful for the construction
materials for such tethers. However, there are several significant
advantages KESTS have in the relatively near future time frame:
first, KESTS do not need development of carbon monofilliament
(diamond monofilliament) tether material before construction;
second, KESTS do not need to be built starting at GEO; third,
tethers are unlikely to have the enormous transportation capacity
to relocate the 1,000,000 people per day necessary to shift civilization
to the OHR; and fourth, perhaps most importantly, KESTS inherently
distributes the transportation energy needed to move payload along
their length, without wires.
Basic Psychological Challenges to the Project
Would mankind choose to endure the massive change of commitments
in nearly every field of human endeavor, rising above entrenched
technologies and cultures, which would be required during the
move of most of civilization to the Orbital Habitat Ring site
as transported by KESTS, even to save their civilization and the
Earth's ecosystem? It is so very difficult to get out of the entrenched
ways of life; the familiar is more predictable and thus seems
more comfortable; and change produces a sometimes unwelcome stress
of striving to cope with the unexpected. Yet we do choose to buy
new clothes, new computers, new cars, new homes. So perhaps we
will also choose KESTS to Orbital Habitat Rings around our precious
Earth.
Unprecedented universal levels of goodwill and cooperation will
be necessary to fully complete the KESTS to OHR project, from
the direct personal level to the international level. Mankind
will need to reach new heights of wholesome cooperative work toward
mutual goals, and stay there. Like Eskimos in their umiak, we
survive through Methexis participation.12
Performance Characteristics
1. On KESTS, vehicles traveling between Earth surface and Earth
orbital altitudes do not carry propulsion fuel. This contrasts
with conventional chemical fueled reaction engine powered launch
vehicles which must utilize the great majority of their lift capacity
to lift the fuel necessary for orbital insertion. Also, conventional
vehicle return to earthsurface requires energy-wastful heat-shielded
dissipation of vehicular energy during the atmospheric reentry;
but during deceleration of vehicular mass during return to earthsurface
along KESTS occurs, the electromagnetic braking force supplies
lift energy to the KESTS and thus returns energy back into the
transportation system.
2. KESTS distribute vehicular propulsion electrical power all
along their structures, without resistive losses of electrical
wiring, and without sliding electrical contacts to extract power
for propulsion, since propulsion energy is coupled inductively
from the mass stream's pulsing magnetic fields.
3. KESTS would somewhat resemble an electric railway-carrying
bridge structure.
4. Powered by electrical energy. Sources of this electrical power
could include existing electrical commercial power grids, "conventional"
SSPS in GEO, and Mass Stream Solar-Electric Thrusters on the KESTS.
The latter two sources may additionally be able to supply electrical
power back into the earth surface electrical commercial power
grid.
5. KESTS would be "active" structures, analogous to a kind of
airplane that is piloted high in the sky while propelling itself
by pushing on the ground below it. Stability is highly dependent
on servo position feedback mechanisms which strive to predict
load transients and compensate for them in advance by appropriate
changes in the exit velocity vectors of the counter rotating mass
streams at the Earth surface re-initialization site; these advance
compensations would ripple through the KESTS at mass stream velocity.
Milestones
1. Milestone one is the successful fabrication and operation of
working models of KESTS which incorporate all of the functions
needed by full scale KESTS. At the present time, work needs to
be done in envisioning potential capabilities and associated side-effects,
such as contemplated by this paper. Much work could soon be done
in the mathematical analysis of suborbital mechanics and engineering
design, relevant electromagnetics and materials technology, with
electronic servo concepts readied for use in automatic adjustment
due to varying loads along the length of the KESTS. Modular armature
segments need to be somewhat standardized providing as small a
stream size as is practical, and providing for bundling many of
these small ones to provide the higher carrying capacity of a
particular application. Enough technology needs to be developed
to build demonstration functional models for people to look at
and touch, perhaps to ride upon.
4. Creation of KESTS surface-to-surface bridges to develop the
technology into a high reliability system, while also providing
new modes of long range transportation of large amounts of fuels,
water and other resources. Development of emplacement techniques.13
2. Since the primary need for KESTS technology is to enable the
Orbital Habitat Rings existence and the transportation of a great
number of people and their belongings to it, perhaps the most
difficult milestone is when humanity realizes there is a choice,
and chooses to go for the gold.
3. The next milestone is the actual proving out of the concept
of nearly self-sufficient artificial large habitats in space,
the demonstration that the complex intertwining mechanical, biological
and sociological systems can harmonize fully adequately. Preassembled
sections of a 1,000-person toroidal research space habitat design
are put into Low Earth Orbit by the creation of a flyback engine/control
type wet launch module vehicle technology, using the existing
proven technology base used for the Space Shuttle development.
The wheel-shaped space habitat is first built on the ground in
the form of pre-fitted modules linked in a mile-diameter circle.
The design of each module is for dual use, the other use is for
being the fuel tank of an unmanned engine & control module vehicle
which launches them into Low Earth Orbit. The unmanned engine/control
module flies back to the launch site for the next module's launch,
much as the present space shuttle returns to the Earth's surface.
Use these unmanned wet-launched prefitted modules to build artificial
gravity space habitats made of circles of these linked modules
to prove out the hypothesis that Earth surface gravity and atmospheric
pressure in a rotating toroid can provide functional stability
in a group living situation which includes other life forms in
a harmonious synthesis. 14
5. First adequately shielded space habitat in GEO Orbital Habitat
Ring a 10,000-person space settlement built from Earth materials,
brought up on a KESTS bridge. This develops the functional structural
design with components built comparatively easily on the Earth's
surface. Outfitting the interior of the space settlement to include
as many earth-normal features as possible. Tests out agricultural
systems, condominium homes on the interior slopes, and creative
harmonious social systems, and millions of the other things needing
to be tested out there too. In a reference design of 1976, each
colonist effectively has 26 fish, 6.2 chickens, 2.8 rabbits, and
1/7 of a cow, and the plant diet for these animals is grown on
the habitat in lunar soil about 1 foot deep. Housing of the colonists
is on terraced condominiums along the sides slopes inside the
rotating wheel habitat, including 45 square yards per person for
residential and community life, 5 square yards per person for
mechanical and life support systems, and 21 square yards per person
for agriculture and food processing.15,16
6. Long term electrical power to support the kinetic energy bridges
needs to come from space resources instead of relying on Earth
resources. Dedicated SSPS in GEO is one possibility; solar- electric
mass stream thrusters hanging on KESTS is another possibility.
Thrusters would use solar energy converted into electrical energy
to accelerate the downward direction of the kinetic mass stream
so as to replenish the energy consumed by the support of the bridge
structure and for moving payloads along it. The thrust of that
acceleration would be against the weight of the power converter,
being located along the bridge at points below synchronous orbit.7
7. The bulk of the physical structure to be built in the Clarke
Belt around the Earth would need to be built out of space resources.
The Moon is handy and has plentiful resources of such materials
as aluminum and titanium. Transport this material from the Moon's
surface to the vicinity of the site for the Orbital Habitat Ring,
efficiently and with a minimum of pre-industrialization of the
Moon: investigate forms of materials-pumps utilizing the greater
depth of potential energy of the adjacent Earth's gravity well,
to lift materials up out of the Moon's gravity well. One way to
do this is to store the energy as angular momentum: an Earth-Moon
two-body orbiting Skyhook one-direction materials pump, which
picks up packaged payloads from the far side of the Moon on a
tether, payload and spacecraft tethered whirling together around
their common center-of-gravity as they continue around the Moon
and into Earth's gravity well, the spacecraft regaining its energy
through appropriately timed release of the payload from a lengthened
tether deep into Earth's gravity well. This concept draws from
Hans Moravecs creation of the spinning Skyhook concept. Lunar
mass drivers, and lunar elevator tethers through L1 are other
technologies worthy of consideration for this purpose.17,18
8. Successful full-size fully functional habitats built on site
in Earth orbit from lunar construction materials, such as the
10,000-person toroidal design.
9. Robotically-built basic habitat shell structure made on site
at OHR altitude out of lunar materials.
10. Sustainable construction rate of 300 orbiting habitats robotically-built
per day in the OHR from lunar/asteroidal raw materials.
11. First million square kilometers of earthsurface restored back
into pre-civilization ecosystem state.
12. Construction/population of second Orbiting Habitat Ring, populated
by 7 billion descendants of first habitat ring's thriving growing
population.
13. Complete restoration of the earth surface ecosystem back to
nearly pre-civilization conditions, with a rotating population
of only 100 million people on the Earth surface at any one time,
composed of ecosystem restoration and maintenance workers, and
national park vacationers.
Safety and Reliability Issues
Safety and reliability of KESTS structures is a primary consideration
of the concepts application. Not only to that which might be
injured by falling pieces of damaged KESTS, but also to other
KESTS, to the people and payload on the KESTS at the time, and
to those dependent on KESTS-delivered products both in the Orbiting
Habitat Ring and on the Earth surface. Aircraft crash liability
and shipping liability models may be starting points for these
issues. It is hoped that empirical experience in developing this
technology will minimize these substantial risks; and the use
of KESTS seed emplacement and bootstrapping construction processes
will start with small risk, and thereafter gain confidence with
experience and growing size of the first KESTS being built to
GEO. The seed KESTS are envisioned preferably as being of tubing
size a small fraction of an inch in diameter, minimizing possible
damage worldwide upon its fall in a developmental testing crash
of a seed KESTS.
Some Research Questions
1. Stability of the KESTS structure: how high can it go while
remaining able to cope with unbalanced transient forces upon it?
What are those expected forces? How much wobble will be present
at any point along it, particularly at the site of embarkation
to the habitat ring? Can its active position servo system be adequately
damped to prevent uncontrolled oscillations in the feedback loop?
What is the ratio of active feedback damping vs. energy-consuming
passive damping structures distributed along KESTS?
2. What is the traffic volume necessary for a given size KESTS,
at the break-even point, considering the energy input required
just to maintain support of the structure?
3. Pulsing magnetic fields present a hazard to living beings:
The coupling of the mass stream to the enclosing tube structure
and to vehicles moving along the structure is primarily of a pulsing
electromagnetic nature. What hazard does this present to passengers,
since some studies have linked such ELF fields to diseases such
as alzeheimers and leukemia; can design minimize such ELF fields
in cargo and passenger parts of the vehicles?
4. What kind of industrial business system can possibly remain
responsible to the long term goals of an expanding civilization
and restoration of the earth surface ecosystem?
5. Willingness of the majority of present-day Earth surface population
to leave their lifelong homes to migrate to the orbiting habitat
ring: people are attached to the familiar, and often have worked
much of their lifetime to provide the home they now live in with
their family, and are not likely to easily choose to leave it
all. The value of their real estate will need to be adequately
returned to them somehow in the overall process. And those whose
fortunes are dependent on the real estate wealth they have currently
amassed, will need assurance of equivalent wealth in the new civilization
site somehow. Who will provide the money for all this? Can there
be a one-for-one correspondence of real estate on the ground with
real estate in the habitat ring? And can life in the habitat ring
be guaranteed sufficiently better than that on earthsurface to
provide the incentive to migrate? 1
6. Can there be multiple KESTS, or would the crossover sites provide
risk of crashing together in space? Can these crossover points
be made deliberately coupled, even providing additional stability
to the overall KESTS system?
7. What effects of the mass streams electromagnetic flow within
the earths magnetic field?
8. The entire KESTS structure must rotate once every 24 hours,
as it is attached solidly to the earth surface. Lateral coupling
between upward and downward mass stream provides the mechanism
to swing the enclosed mass streams around with the rotation of
the earth, but what are the magnitudes of the distributed lateral
force between the mass streams and tubing, and how much weight
does this structure add to the KESTS? These are important parameters
for KESTS equations.
9. Given the transfer of most of most of civilization to the Orbital
Habitat Rings around the Earth, 15 billion people in the hypothetical
example given here illustratively, there would be plenty of spare
mile-diameter 600 feet wide toroidal habitats, which could be
used to re-create small copies of earthsurface natural ecosystems.
Those local zoological parks conceivably could be ark-like backups
for all of the original earthsurface species, including the largest
land and marine mammals. Those space-based zoological gardens
would be excellent research sites for the restoration and maintenance
of the giant national park that the earthsurface could become,
preserving precious biological genetic resource pools of biodiversity
for the future. What will be the managerial processes that ensure
this will happen?
In Conclusion
Kinetic Energy Supported Transportation Structures potentially
have some interesting properties, primarily as a supportive structure
for efficient electrically powered rail transportation, and also
as a distributor of transportation energy along itself, as an
energy storage system, and possibly as a provider of space solar-derived
electric power to earthsurface commercial electric power grids.
The compressive strength of these enormous structures bridging
between earthsurface and space is greatly augmented by radially
compressing supra-orbital velocity mass streams whirling within
a bridging structure around the planet, their outward centrifugal
force providing primary support for the weight of the enclosing
tubing structure and its associated track and vehicle system;
electromagnetic drag against the high velocity rising armature
mass stream providing distributed support of the weight of the
earthsurface-stationary parts of the structure. Similarly, vehicular
propulsion energy is electromagnetically coupled from the armature
mass stream to vehicles carrying payload along tracks on its tubing,
thus lift energy is distributed intrinsically to the point of
need. Only a small fraction of kinetic energy within the mass
stream is consumed per transit loop, so there is much energy stored
in the system, providing some resiliency. KESTS to GEO would provide
the lift capacity for building large scale Solar Satellite Power
Stations in GEO, thus providing electric power for itself and
for sale to others; additionally, solar-electric powered mass
thrusters mounted on the KESTS itself may be able to input power
enough to maintain support of the KESTS and provide surplus electric
power for use on Earth surface electric power grids, delivered
by the mass stream instead of by microwave energy. Bootstrapping
construction from seed KESTS which is emplaced by mass stream
nose thrust-reversing flyable versions is described as one emplacement
technique for these massive structures. A KESTS configuration
for direct access from higher earth latitudes is described, utilizing
surface contact points which are mirrored about the equatorial
plane. KESTS concepts suggest to us a way to move ourselves and
our civilization's belongings far and high into Earth orbit, enabling
earth life to massively occupy the relatively motionless orbit
of the Clarke Belt. The decision to research and develop the technology
of kinetic energy supported electrically powered transportation
structures would be a major step toward true large scale colonization
of space, preserving a vigorous expanding civilization and restoring
the Earths surface ecosystem at the same process, hopefully beginning
in our time.
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