|





| |
 |
Impulse Engine |
What Makes It Go
 |
|
Gravity... Lord of Light:
Matter vying for the same space.
Consciousness IS the space.
Matter and space support each other
Like a dream void of substance,
Or a fragile bubble,
Held apart only by a breath. |
|
Steven's derivative
of The Heart Sutra |
How to lose weight without throwing away the ship
– or the passengers
Rockets must lose 90 percent of their weight in fuel just to thrust the ship
into orbit. Sometimes they lose human life. Are there other ways to do this
without the waste and risk? Dean built a centrifugal force engine that lost 5%
of its weight while running on a floor scale.[11] According to many physicists,
even that slight weight loss would have been enough to have made us a
space-faring race. So why aren’t we walking on the Moon and Mars today thriving
with an interplanetary economy?
Sadly for Dean and the rest of us the political atmosphere of the 1950s, and
resistance from the scientific community enchanted with the fireworks of rocket
propulsion, grounded the Dean Drive.[12]
|

Centrifugal force
from a three frame system: Taking advantage of the third derivative
effect. |
The Reciprocating Impulse Drive (RID)
Inertial propulsion engine E-8 is a two-cycle, 10 Hz reciprocating impulse drive
(RID). It weighs 40 lbs and loses over 27 lbs while running on a floor scale
(two different brand-name bath scales) without ejecting mass - using just 160
watts of power. This is a steady weight loss, not a bouncing scale or resonating
dial effect, from a dependable centrifugal force engine that will not fly apart.
Though my earlier inertial propulsion prototypes run horizontally using
“stick-slip” (friction as a back-stop) because they are single-cycle units (E-4
and E-6), a multiple-cycle unit like RID can overcome its inertia vertically
because there is no time for “slip”. Also, in-line spring-loaded floor scales
have no “stick” to them. To top it off, this engine has built-in acceleration
detectors that unmistakably display continuous thrust on the front panel. Dust
particles on the top-plate dance so fast, they clearly float above the engine
from the centrifugal force of its whirling “elliptics”.
|

Power supply PS-3
is a custom dual DC power supply for inertial propulsion engine E-8
(RID). Hand-built from scratch by the author in 1992 for E-4, then
beefed up in 1996 for E-8, PS-3 delivers upwards 300 watts if
needed. However, RID uses only about half that to lose over 27 lbs. |
Unlike prior art this drive is lightweight and has no
complicated moving parts to quickly wear-out and break, nor requires regular
lubrication. It runs on man’s most convenient form of power – electricity so it
is clean and quiet. Because RID’s internal forces align with the direction of
travel it’s resilient and dependable.
|
A megavolt solid-state Impulse Drive could cyclically
knock-up electrons of an engineered substrate creating upward drag on its nuclei
for levitation. |
This impulse engine is composed of two carriages that are
suspended by springs on the four rods of a mainframe in-line with a control
platform. Each carriage holds two counter-spinning eccentric rotors of solid
brass weighing 2 lbs each with a 1.5” radius and spin at 300 RPM. This equates
to 5 Hz frequency for each carriage which reciprocates, giving a total engine
frequency of 10 Hz (cps). The direction of rectified force is upwards within the
mainframe.
The Pendulum Test 2009
Like all engines, if the load is not properly placed, efficiency declines.
The load of gravity on the engine's carriages (as weight) in the vertical
acts differently than when running horizontally because the carriages are
now weightless. We are working on making the adjustments to compensate for
this load change and - for the easy transition between these load changes.
In May 2009 I installed Revision 6 to allow the engine to gain more ground
across the zenith board. See below. The time available to me to work on this
drive is limited, but in the summer of 2011 I will modify the drive
again so that it may carry (not drag) - a load horizontally on frictionless
roller bearing wheels and will publish the results on this site.
 |
E-8 Pendulum Test – June 2009
Inertial Engine E-8 hanging from four 76-inch long, 75 lb-test steel
chains. Reference board is propped-up behind engine and not in
contact with machine. Engine frequency while running on its side is
13 - 14 Hz. |
| |
 |
 |
 |
|
Engine E-8 hanging at rest with its base-plate
bottom edge aligned with thick black line on reference board. |
Engine running and steadily
deflecting from zenith 1-inch plus. Bottom carriage is now providing
thrust. |
Top carriage is now providing thrust. For
reference, the engine base-plate is 3/4-inch thick. |
| |
 |
 |
 |
|
Bottom carriage is about to provide thrust. Note
engine is still deflected from zenith - inertial delay at work. |
Top carriage is providing thrust. |
Both carriages are in transition and engine is
still deflected from zenith.
Photographed with Kodak
DZ1012 IS at 10 mega pixel resolution |
Electric Satellite Engine
Because satellite orbits decay and sometimes need to be moved about, they
require large tanks of retro jet propellant or dangerous nuclear batteries. This
means extra weight, space, and limited life. As such, there is an open market
for an efficient, electric satellite engine. The required impulse drive doesn’t
have to become totally weightless on the ground but it should lose substantial
weight while running. RID is a working prototype of such a drive.
The RID’s steady weight-loss equates to about 70% of the engines’ weight and
would be like a 185 lb man in orbit suddenly reducing his weight to 55 lbs; he
would be shot through space with 130 lbs of thrust. In this case, the engine
would propel itself and anything attached to it with 27 plus lbs of thrust.[13]
But this is more than enough force to maneuver a two-ton satellite in orbit.
Mounted in a 360-degree gimble and guided by a radio-controlled joystick this
engine could place an orbiting satellite anywhere – even into deep space and
beyond – using solar or nuclear power. Since this drive functions with five
separate inertial frames (it has two carriages) it’s exceptionally efficient at
160 watts avg. or just 1/5th hp.
|

Brass vs. Tungsten Rotors:
Both rods are the same height, 3.5”. On the left is a brass rod 1.0”
diameter and weighs 375 gr. On the right is a .9375” diameter sample
tungsten rod weighing in at 669 grams - almost twice as much as the
slightly larger brass rod. Tungsten is usually refined as a powder,
then cast and compressed under high temperatures. It machines like
cast iron and comes in “one inch” diameter rods as shown above –
ideal for Dean Drive rod-rotors because the massive bars take up
less space, resist corrosion and keep a high sheen for low
aerodynamic friction. Because of the prohibitive cost of tungsten,
E-8 has brass rotors. |
Mission to Mars
The RID was designed to lose weight only and impel payload already in orbit.
However, from the Moon’s surface RID would lift-off and attain orbit with 20 lbs
of thrust because the Moon’s gravity is one-sixth g. Though the weight of the
engine and its rotors are reduced, the rotor's inertial mass are not and
provides the same force as on Earth (a dumbbell in space has the same
intractance as it does on Earth but without the weight). From the surface of
Mars RID would lift-off with 12 lbs of thrust, Mar’s gravity being about
one-third g.
|

The Balance Beam Test:
Though a dramatic demonstration, this test is too demanding on the
prototype and stresses gears and linkages to the point of breakage;
Even though it is a rigid beam, the engine has to work against the
reactive bounce-back of the beam from the weight stack with every
impulse. |
Mars’ orbit swings it close to Earth once every two
earth-years where there is a 6-month window of space travel. With conventional
rocket powered spacecraft a manned trip to the red planet would take the full 6
months, then a 12-month wait for the orbits to conjunct again, then another
6-month trip back home to Earth.
Eight RID engines (8 E-8’s) ganged together in free space could safely thrust
humans to Mars within a month at a fraction of the cost of dangerous rockets.
Once activated, in a short period of time, the spacecraft would impel smoothly
to a very high rate of speed. To slow and brake the craft, the 16-cycle engine
would simply be turned 180º then reactivated – all mounted safely inside the
ship for ease of maintenance and omni-directional control.
| A |
B |
 |
 |
| E-8 weighing 40 lbs |
E-8 weighing 13 lbs |
| Out-Running Gravity |
|
A.
Engine at rest and loosely tethered RID on standby weighs 40 lbs and
adaptor table weighs 9 lbs totaling 49 lbs. Note position of brass
rod-rotors and spacing between the carriages. |
|
B. Engine is running with carriages
desynchronized (180°out of phase with each other, or normal phasing)
producing a steady weight loss of over 27 lbs, the scale resolving
at under 22 lbs. Note brass rod-rotor’s position relative to
carriages (also with engine off, these heavy rotors would normally drop
and not rest horizontally). Unfortunately camera flash overwhelms
the LED indicators on the control panel. Photographed with Kodak 200
speed film. |
Slingshot to Saucercraft
Shortly after the dawn of man – long before we invented the wheel – we harnessed
the centrifugal force of the rotary slingshot. Since then there’ve been no
further developments of the potential energy that physics terms “angular
momentum”. It has remained locked up in rotary motion. Hold a spinning gyroscope
and twist it perpendicular to its plane of rotation and you’ll feel a delayed
but powerful reactive force between its two inertial frames. This is the
potential that is temporality stored in angular momentum. But in gyroscopes and
flywheels this potential is spread evenly about the rotor’s orbit.
|

Electric Flight:
Concept drawing of a trans-orbital electromagnetic hovercraft
utilizing radial vectored rotors to produce lift. A Ferro-fluid
guidance system about the perimeter tilts the craft in the direction
of destination and also by slowing down the rotors in that quadrant.
The radar dome on top of the canopy also houses the emergency
parachute and a communications link. Solar panels line the top half
of the craft to help power the electric saucer. |
Eccentric rotors, on the other hand, do not have a
smooth, even angular momentum so can be configured into oscillatory motion
whereby surge can manifest along the plane of rotation. Then, by shifting this
two-frame oscillator complex within its third-frame housing to increase the CAT,
angular momentum can become kinetic and the rotor’s centrifugal force is no
longer balanced by a centripetal. For a brief moment in an eccentric rotors’
cycle, these two opposing forces are separated and a powerful burst of energy is
efficiently released at the expense of electricity. One day soon – like the
horse and buggy – tires, roads and bridges will be remnants of the past, thanks
to Norman L. Dean's inertial propulsion drive.
Steven M. Hampton
Chief Engineer
Centrifugål Dynamics Co.
email: Thrust@frontiernet.net
|
Those who
have contributed to the development of these engines: |
| Norman L. Dean |
| William O. Davis, PhD |
| G. Harry Stine |
| Norman Parrish, PhD |
| John Campbell, Jr. |
| Craig “T” Herrington |
| Sensei John Angelos |
| Cris Angelos, PhD |
| Lucjan Shila |
| Thomas Valone, PhD |
| Kent Hanna |
| Larry Goff |
| Robert Moreno |
| Gary French |
| And many others
too numerous to mention... |
Endnotes / Bibliography
[11] John W. Campbell, Jr., The Space Drive Problem,
Astounding Science Fact and Fiction, June 1960, pg 98.
[12] John W. Campbell, Jr., That Fourth Law of Motion, Analog, May 1962, pgs 4
-6, 177.
[13] Like any other form of propulsion, inertial engines need a load or enough
mass to stabilize the mainframe of the drive. In the case with RID’s weight loss
demonstration gravity is the load. In space it would be the inertial mass of the
satellite or spacecraft that would provide the load.
Photographs and drawings by Steven Hampton © 2007, 2011

| |
|