U.S. patent number 3,916,761 [Application Number 05/438,147] was granted by the patent office on 1975-11-04 for two stage light gas-plasma projectile accelerator.
Invention is credited to James C. Administrator of the National Aeronautics and Space Fletcher, Eduard B. Igenbergs, David W. Jex, N/A, Edward L. Shriver.
United States Patent |
3,916,761 |
Fletcher , et al. |
November 4, 1975 |
Two stage light gas-plasma projectile accelerator
Abstract
A device for accelerating a projectile to extremely high
velocities includes a light gas accelerator to impart an initial
high velocity to the projectile and a plasma accelerator and
compressor receiving the moving projectile and accelerating it to
higher velocities. A capacitor bank is discharged into a plasma
generator in timed relationship to the position of the projectile
so that the moving plasma drags the projectile along with it.
Projectile velocities in the order of 20 kilometers per second, the
average meteoroid velocity, can be attained, whereby the
accelerator finds particular utility in the field of meteoroid
simulation.
Inventors: |
Fletcher; James C. Administrator of
the National Aeronautics and Space (N/A), N/A
(Huntsville, AL), Shriver; Edward L. (Huntsville, AL),
Jex; David W. (Guntersville, AL), Igenbergs; Eduard B.
(Munich, AL) |
Family
ID: |
23739436 |
Appl.
No.: |
05/438,147 |
Filed: |
January 29, 1974 |
Current U.S.
Class: |
89/8; 73/12.11;
315/111.61 |
Current CPC
Class: |
F41B
6/00 (20130101) |
Current International
Class: |
F41B
6/00 (20060101); F41F 001/04 () |
Field of
Search: |
;89/7,8 ;73/12
;315/111,111.5,111.6 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Bentley; Stephen C.
Attorney, Agent or Firm: Porter; George J Wofford, Jr.; L.
D. Manning; John R.
Government Interests
ORIGIN OF THE INVENTION
The invention described herein was made in the performance of work
under a NASA contract and is subject to the provisions of Section
305 of the National Aeronautics and Space Act of 1958, Public Law
85-568 (72 Stat. 435; 42 USC 2457).
Claims
We claim:
1. A device for accelerating a projectile to a high velocity,
comprising:
a light gas accelerator, including a barrel, for imparting an
initial velocity to said projectile;
a plasma generator adapted to receive said projectile from said
barrel, said plasma generator being of the type having a pair of
coaxial electrodes, said barrel extending into said generator so as
to constitute the center electrode thereof;
means for initiating the generation of said plasma when said
projectile is in a preselected location in said generator; and,
means for controlling the flow of said plasma in a manner so as to
accelerate said projectile to velocities higher than the initial
velocity.
2. The device of claim 1 wherein said plasma generator
comprises:
a capacitor bank switchably connected to the electrodes; and,
a thin metal foil disposed between and electrically connecting the
electrodes.
3. The device of claim 1 wherein said plasma flow controlling means
includes a plasma compressor coil of conical shape mounted with the
cone axis coaxial with said barrel with the large end of the cone
adjacent said plasma generator, whereby said projectile travels
along the cone axis from the large to the narrow end thereof.
4. The device of claim 3 further including a dielectric block
mounted on the outer electrode of said plasma generator, and
wherein:
the large end of said coil is affixed to said block; and,
the narrow end of said coil is electrically connected to said outer
electrode.
5. The device of claim 2 wherein said plasma generation initiating
means includes:
a photosensitive device mounted such that the sensitive area views
the exit end of said barrel; and,
switching means for connecting said capacitor bank to said
electrodes in response to a signal from said photosensitive
device.
6. The device of claim 5 wherein said switching means includes
means for delaying the connection of said capacitor bank to said
electrodes for a preselected time following the receipt of the
signal from said photosensitive device.
7. The device of claim 3 wherein said plasma generator
comprises:
a capacitor bank switchably connected to said electrodes; and,
a thin metal foil disposed between and electrically connecting said
electrodes.
8. The device of claim 7 wherein:
the capacitor bank discharge voltage waveform is a damped sine
wave; and,
the parameters of said plasma generator and plasma flow controlling
means are so related to each other and to the projectile dynamics
that the projectile is in the narrow end of the compressor coil
when the discharge voltage begins to decrease.
Description
BACKGROUND OF THE INVENTION
The present invention relates generally to the field of projectile
acceleration, and more particularly to apparatus including a light
gas accelerator for causing a projectile to attain extremely high
velocities.
Many techniques have been used in the attempt to achieve a high
projectile velocity. Many of these efforts have been directed
toward the achievement of average meteoroid velocity with a
relatively small projectile. Projectiles traveling at such a
velocity are very useful in the testing of meteorite damage to
space vehicles and in the simulation of orbital velocity re-entry
problems.
One prior art technique for projectile acceleration is a light gas
accelerator utilizing the compression of a light gas to drive the
projectile by driving a piston through an enclosed pump tube
containing the light gas with a diaphragm at the other end of the
tube. When the diaphragm bursts, the compressed gas accelerates the
projectile down a barrel. While this is a useful technique, the
performance of such a device is fundamentally limited by the finite
velocity of sound in a gas. Thus, at any given time, the gas
pressure near the projectile is only a fraction of the pressure
near the piston, resulting in lower acceleration to limit terminal
velocity of the projectile.
Other methods of projectile acceleration include the use of gases
from chemical explosions, electrostatic potential accelerators,
electrically exploded wires, high velocity plasmas, and
combinations thereof. Some of these methods do achieve the desired
projectile velocity, but are restrictive in the size of the
projectile which can be accelerated. Other of the methods can be
used for a wide range of projectile sizes, but the projectiles
cannot achieve the 20 kilometer per second velocities needed.
SUMMARY OF THE INVENTION
The general purpose of the present invention is to provide a
projectile accelerator that cannot only be used for a wide range of
projectile sizes, but can also provide the projectile with
velocities of 20 kilometers per second or more. To attain this
result, the accelerator of the present invention combines a light
gas accelerator with a high velocity plasma generator in such a
manner that the velocities imparted to the projectile by each are
additive.
The device can be considered as consisting of three component
parts. They are: a light gas accelerator, a plasma accelerator, and
a self-energized plasma compressor. These components are combined
in a manner which allows each component to contribute its unique
capabilities to the overall system performance in accelerating
projectiles.
The light gas accelerator provides the projectile with an initial
velocity. As the projectile leaves the barrel of the light gas
accelerator, a plasma is generated in the region around the barrel.
This plasma is caused to move at high velocity in the same
direction as the projectile is moving. The moving plasma drags the
projectile along with it, accelerating the projectile to higher
velocities. The generation and movement of the plasma is
synchronized with the projectile position.
Therefore, it is an object of the present invention to provide
apparatus capable of accelerating projectiles of a wide range of
sizes to velocities of 20 kilometers per second or more.
Another object of the present invention is to provide a projectile
accelerator which can provide projectile velocities at least as
high as the average meteoroid velocity.
BRIEF DESCRIPTION OF THE DRAWINGS
These and other objects, advantages and novel features of the
present invention will become apparent from the following detailed
description of the invention when considered in conjunction with
the accompanying drawings, wherein:
FIG. 1 shows a preferred embodiment of the present invention;
and,
FIG. 2 illustrates the timing relationship between the plasma
generation and projectile position.
DESCRIPTION OF THE PREFERRED EMBODIMENT
Referring to FIG. 1, a light gas accelerator 1 comprises a
cylindrical pump tube 2 filled with a light gas 3, such as hydrogen
or helium. At one end of the tube is a deformable polyethylene
piston 4. Behind the piston is an explosive charge carrying device
5, such as a conventional 30 caliber rifle cartridge loaded with
gun powder. A firing pin 6 for firing the cartridge is disposed
adjacent the cartridge base.
At the other end of tube 2, a stationary retaining diaphragm 7
seals the tube. The projectile 8 is disposed on the other side of
diaphragm 7 within metal barrel 9, which extends through insulating
member 10 into plasma chamber 11. A tubular conductive member 12 is
mounted on insulating member 10 and is coaxial with barrel 9. A
thin foil 15, of aluminum or some other metal, connects member 12
to barrel 9 within the plasma chamber 11. A conical compressor coil
13 is disposed at the open end of plasma chamber 11 coaxial with
the barrel 9. The coil is of copper wire and is partially insulated
to prevent arc over between windings, but uninsulated on the inner
diameter of the coil. The large end of coil 13 faces the plasma
generator, as shown in FIG. 1, and is separated therefrom by a
dielectric mounting block 14 which holds the coil 13 in a position
coaxial with the plasma generator. The opposite, narrow end of coil
13 is held in position by another dielectric block (not shown)
attached to the plasma generator.
A capacitor bank 16 has one terminal connected via electrical
conductors 17 and 18 to conductive member 12 and to the narrow end
of coil 13 via conductors 17 and 19. The other terminal of the
capacitor bank 16 is connected to a delay generator switch 20, the
function of which will be described below, by electrical conductor
21. Also connected to switch 20 is a photosensitive detector 22,
which can be any one of a variety of photosensitive devices, such
as photomultipliers, phototransistors, etc. The detector 22 is so
disposed that the photosensitive area views the end of barrel 9.
Switch 20 is connected to conductive barrel 9 by conductor 23.
The operation of the device will now be described. The cartridge 5
is fired by firing pin 6 and the expanding gas from the fired
cartridge forces piston 4 to move down the center of pump tube 2,
thereby compressing the gas 3 between piston 4 and stationary
diaphragm 7. The trapped gas increases in pressure until a pressure
is reached which causes the retaining diaphragm 7 to burst. The
pressure is a function of the thickness of the diaphragm. After the
retaining diaphragm has burst, the escaping, high pressure, hot gas
accelerates projectile 8 down barrel 9. The barrel serves a
multipurpose in this device. It serves to confine the escaping gas
and accelerate the projectile, it serves to aim or direct the
projectile toward the target, and, as will be described below, it
serves as one electrode of the coaxial plasma generator.
The projectile exits from barrel 9 at some initial velocity in a
direction coaxial with the plasma generator and with the compressor
coil 13, and in the direction of the target which is to be impacted
with the projectile. When the projectile is free of the barrel, and
at a time appropriate for the plasma generator and compressor coil
to exert their maximum effect upon the projectile, the electrical
energy stored in capacitor bank 16 is discharged into the coaxial
plasma generator. As described above, one terminal of the capacitor
is connected to conductive member 12 while the other terminal is
connected to conductive barrel 9 through switch 20. When switch 20
is closed, a very large current flows through metal foil 15,
evaporating the metal and creating a metal plasma. The plasma so
produced is acted upon by the forces arising from the interaction
of the current in the metal plasma with the magnetic field of
center electrode 9. This force causes the plasma to be accelerated
out of the plasma generator 11 and into the plasma compressor coil
13. When the expanding metal plasma contacts the uninsulated inner
portions of compressor coil 13, a current is established in the
coil which creates a time changing magnetic field in the
longitudinal direction. The current generated in the plasma by the
time varying magnetic field flows perpendicular to the field. The
force on the plasma is, then, radially inwards. A dynamic balance
is attained between the current in the coil 13 giving rise to the
magnetic field and the force on the plasma so that the plasma is
contained within the coil during the increasing current phase of
the discharge. When the current from the capacitor bank 16 starts
to decrease, the magnetic field in the coil maintains its direction
but starts to decrease. This causes the current induced in the
plasma to change direction, forcing the plasma out of the coil. At
the time the magnetic field starts to decrease, the projectile is
at the narrow end of the coil and is accelerated to a higher
velocity by the expanding plasma.
The use of a proper time delay between the firing of the light gas
accelerator and the discharge of the capacitor bank is important to
the attainment of average meteoroid velocities by the projectile.
For maximum velocities to be attained, the plasma generation must
be synchronized with projectile position. Since the characteristics
of the light gas accelerator are known, a time delay measured from
the cartridge ignition time could conceivably be utilized. However,
it has been found in practice that such a method is not
satisfactory due to the fact that the time between cartridge
ignition and projectile exit from the barrel varies over too wide a
range. It has also been found in practice that the light gas
accelerator emits from barrel 9 a flash of hot gas a predictable
length of time prior to the exit of the projectile from the barrel.
The phenomenon is utilized to synchronize the plasma with the
projectile by means of photosensitive device 22 and delay generator
switch 20. The photosensitive device 22 detects the emission of hot
gas from the barrel and initiates the operation of a time delay
circuit. At the conclusion of the delay period, switch 20 closes
and applies the energy in the capacitor bank 16 to the plasma
generator.
FIG. 2 illustrates the desired relationship between the projectile
position and the capacitor bank discharge current, which is shown
as a damped sine wave. At point A, the switch 20 has just closed
and the capacitor bank 16 has just begun to discharge. At this time
the projectile should have just left the barrel 9 and entered the
plasma generator. At point B, the first half cycle of the sine wave
capacitor discharge current has peaked and is starting to decrease
in amplitude, although the polarity is still positive. This is the
time mentioned above when the plasma current changes direction and
the plasma expands out of the coil. At point B, the projectile
should be near the narrow end of the coil 13 so as to be
accelerated out of the coil by the expanding plasma.
Obviously, the period of the capacitor bank discharge sine wave,
the dimensions of the plasma accelerator and compressor coil, the
initial velocity imparted to the projectile, the size, shape and
weight of the projectile, as well as many other factors, are
variable and under control of the designer. Therefore, it is clear
that many modifications and variations of the present invention are
possible in light of the above teachings. It is to be understood
that, within the scope of the appended claims, the invention may be
practiced otherwise than as specifically described.
* * * * *