U.S. patent number 3,680,130 [Application Number 04/875,879] was granted by the patent office on 1972-07-25 for re-entry vehicle nose cone with antenna.
This patent grant is currently assigned to The United States of America as represented by the Secretary of the Army. Invention is credited to Howard S. Jones, Jr., Harry K. Morlock, Joseph J. Witte.
United States Patent |
3,680,130 |
Jones, Jr. , et al. |
July 25, 1972 |
RE-ENTRY VEHICLE NOSE CONE WITH ANTENNA
Abstract
Disclosed is a re-entry vehicle in the form of a nose cone body
having an electrically conductive outer surface free of
discontinuities and incorporating an antenna for exciting the body.
The antenna is adjacent the vehicle base where the plasma layer
during re-entry is a minimum. The antenna is disclosed as recessed
into the base surface of the body.
Inventors: |
Jones, Jr.; Howard S.
(Washington, DC), Witte; Joseph J. (Silver Spring, MD),
Morlock; Harry K. (Washington, DC) |
Assignee: |
The United States of America as
represented by the Secretary of the Army (N/A)
|
Family
ID: |
25366528 |
Appl.
No.: |
04/875,879 |
Filed: |
November 12, 1969 |
Current U.S.
Class: |
343/708; 343/769;
343/789; 343/899; 343/767; 343/770; 343/873 |
Current CPC
Class: |
H01Q
1/281 (20130101) |
Current International
Class: |
H01Q
1/28 (20060101); H01Q 1/27 (20060101); H01q
001/28 (); H01q 013/10 (); H01q 013/18 () |
Field of
Search: |
;343/700,705,708,711-717,767-779,872.3,895.9,784,789 ;102/7.2P
;244/3.11,3.13,3.14,3.19 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Other References
"Lightweight Ceramics Seen As Ideal for Radomes," Metzger in
Ceramic Induies June 1957 TP 785 C411; pages 122, 123, and
135.
|
Primary Examiner: Lieberman; Eli
Assistant Examiner: Nussbaum; Marvin
Claims
What is claimed and desired to be secured by United States Letters
Patent is:
1. A re-entry vehicle comprising a body portion having an outer
surface substantially free of surface discontinuities which
terminates in a base surface having the shape of a slice of
cross-sectional area of said body portion, said base surface
including a hemispherical recess and said antenna comprising a
top-loaded monopole antenna mounted in said recess.
2. A re-entry vehicle comprising a body portion having an outer
surface substantially free of surface discontinuities which
terminates in a base surface having the shape of a slice of
cross-sectional area of said body portion, an antenna for exciting
said body portion recessed in said base surface, said antenna
comprising a pair of radiative, resonant, wave guide cavities
extending in one direction in the longitudinal axial direction of
said body portion and extending in the other direction arcuately
about the longitudinal axis of said body portion.
3. A re-entry vehicle comprising a body portion having an outer
surface substantially free of surface discontinuities which
terminates in a base surface having the shape of a slice of
cross-sectional area of said body portion, a protective radome
comprising part of said body portion, an antenna for exciting said
body portion being recessed in said base surface and being mounted
on said radome and wholly contained beneath the surface of said
radome, said antenna comprising a conductive ring having a radially
inner side on the inner wall of said radome and a radially outer
side embedded in said radome, and including an annular slot in its
radially outer side for radiating electromagnetic energy outwardly
through a portion of said radome.
4. A re-entry vehicle according to claim 3 including an annular
window in said radome surrounding said slot and transparent to
microwave energy.
Description
The invention described herein may be manufactured, used and
licensed by or for the United States Government for governmental
purposes without the payment to us of any royalty thereon.
This invention relates to the incorporation of various antennas
into the structure of a re-entry vehicle to excite the vehicle body
for radar and other applications.
Conventional constructions for exciting missile bodies generally
employ stubs, monopoles, dipoles and loops as radiating elements.
However, apertures for the antennas and other discontinuities
constructed into the surface of the missile structures for these
types of excitation elements often produce undesirable aerodynamic
effects and changes in the missile's radar cross sectional area
which can be extremely detrimental to the radiation pattern and to
the operation of the missile system. It is therefore desirable to
construct an excitation antenna for a re-entry vehicle which
permits the surface of the vehicle body to be uniform and free from
discontinuities. At the same time, during re-entry the plasma
environment surrounding the re-entry vehicle has a serious affect
on the antenna and on its radiation characteristics.
The present invention avoids the above-mentioned difficulties by
providing a re-entry vehicle in which the excitation antenna is
recessed within the vehicle body to provide a body surface that is
uniform and free from discontinuities. In the present invention,
the antenna is formed at or near the rear or base of the re-entry
vehicle where the ionized layer surrounding the vehicle during
re-entry is a minimum so that it has a minimum effect on the
radiation characteristics of the antenna.
It is therefore one object of the present invention to provide a
re-entry vehicle having improved electromagnetic radiation
characteristics.
Another object of the present invention is to provide a re-entry
vehicle having a body uniform and free from discontinuities and a
substantially constant radar cross sectional area.
Another object of the present invention is to provide a re-entry
vehicle in which the excitation antenna is recessed and located at
or near the base of the vehicle.
Another object of the present invention is to provide an improved
excitation antenna construction for re-entry vehicles or nose
cones.
Another object of the present invention is to provide an improved
re-entry vehicle in which the excitation antenna for the vehicle is
incorporated in the re-entry vehicle radome wall.
These and further objects and advantages of the invention will be
more apparent upon reference to the following specification,
claims, and appended drawings, wherein:
FIG. 1 is a perspective view of a re-entry vehicle or nose cone
constructed in accordance with the present invention with the
radome shown in cross section for the purposes of explanation;
FIG. 2 is a rear view of the re-entry vehicle of FIG. 1;
FIG. 3 is a partial cross section through the base of the re-entry
vehicle of FIG. 1 showing the hemispherical shape of the recess in
the vehicle base;
FIG. 4 is a partial perspective view of the re-entry vehicle
similar to that of FIG. 1 incorporating a modified excitation
antenna in the form of a pair of recessed waveguide cavities;
FIG. 5 is a rear view of the re-entry vehicle of FIG. 4;
FIG. 6 is a partial cross section through a re-entry vehicle radome
showing a modified excitation antenna for a re-entry vehicle;
FIG. 7 is a perspective view of the radome of FIG. 6 with the outer
section of the upper end of the radome removed for clarity;
FIG. 8 is an elevational view of a radome constructed in accordance
with FIGS. 6 and 7 but incorporating a transparent microwave window
in the outer section of the radome base; and
FIG. 9 shows a typical radiation pattern for a re-entry vehicle
constructed in accordance with this invention.
Referring to the drawings, FIGS. 1-3 show a re-entry vehicle,
generally indicated at 10, in the form of a more or less
conventional nose cone or vehicle body 12 having an electrically
conductive metallic outer skin and surrounded by or enclosed by a
relatively thin layer of dielectric 14 forming a heat shield or
radome for the vehicle. The radome is preferably formed of quartz
or other suitable insulating material.
The surface base 16 forms the base of body portion 12 and is formed
with a central hemispherical recess or cavity 18 aligned with the
longitudinal axis 20 of the re-entry vehicle 10. Extending upwardly
from the bottom of recess 18 along axis 20 is an antenna 22,
preferably in the form of a top-loaded folded monopole. Monopole 22
is constructed so that it does not extend beyond the plane of the
base 16 of the vehicle body so that it does not project from the
body where it may be adversely effected by the plasma layer
surrounding the body during re-entry and even wholly or partially
burned off by the excessive heat to which the body may be subjected
during re-entry.
FIGS. 4 and 5 show a modified re-entry vehicle construction,
generally indicated at 30, again comprising a body having a base 32
and surrounded by a radome insulating layer 34. The re-entry
vehicle 30 is similar to that shown in FIGS. 1-3 with the exception
that the base 32 has formed in it a pair of arcuate recesses or
cavities 36 and 38 forming a pair of waveguide cavities. Each of
the cavities 36 and 38 is slightly spaced radially inward from the
outer edge of the base of the vehicle body and extends
approximately 150.degree. about the vehicle axis. It is desirable
to use as much of the surface area available commensurate with the
operating frequency of the antenna formed by the waveguides 36 and
38 and each cavity may extend as much as about 170.degree. about
the axis. The cavities may be excited in anY conventional manner,
such as by a center probe or loop and are preferably excited in
phase from a common source.
FIGS. 6-8 show a further antenna modification for exciting the body
of a re-entry vehicle. In this embodiment, the antenna is formed in
the radome surrounding the vehicle body and for the sake of
clarity, the body itself which the radome surrounds has been
omitted from FIGS. 6-8. Referring to those FIGURES, a radome,
generally indicated at 40, adapted to surround a re-entry vehicle
body, such as the body 12 of FIG. 1, is provided with a lower
section or nose section 42 and an upper or base section, generally
indicated at 44. The two sections of the radome, which typically
may be formed of suitable insulating material such as quartz from
about one-half to about 1 inch thick, may simply be formed by
slicing off the base of a conventional radome along a horizontal
plane as indicated by the separation line at 46.
Base section 44 of the radome 40 is cut longitudinally to form two
concentric sections comprising outer section 48 and inner section
50. Inner section 50 is provided with a conductive metal coating,
such as copper plating as indicated at 52, over its entire surface
to form a dielectric loaded annular or ring antenna. After the
inner section 50 has been copper plated or similarly coated with a
layer of electrically conductive material, an annular ring 54 is
cut into its outer surface about halfway through inner section 50.
This ring forms a radiating slot for the dielectrically loaded
annular antenna and after the ring has been cut into the radial
center section 50, it is then slipped back inside outer section 48
and the two sections suitably joined together and to the lower
section 42 of the radome. The radome may then be placed over and
secured to a vehicle body, such as the body 12 of FIG. 1. However,
in this embodiment, the excitation antenna is formed in the radome
and no antenna, such as the monopole 22, is required on the vehicle
body itself. In the event the radome 40 is made from a material
other than quartz, then the outer section 48 of the radome may be
provided with an annular quartz window 56, as illustrated in FIG.
8, through which energy from the annular antenna may radiate
outwardly of the radome, i.e., the quartz window 56 should be in
radial alignment with the radiating slot 54 of the antenna.
It is apparent from the above that the present invention provides
an improved construction and arrangement for incorporating an
excitation antenna in a re-entry vehicle subject to the severe heat
and plasma environments which such a vehicle undergoes during
re-entry into the earth's atmosphere. Important features of the
invention include recessing the antenna into the body of the
vehicle or incorporating it in the radome so as to preserve the
smooth and unobstructed surface which the vehicle must have to
avoid undesirable aerodynamical effects. In addition, the vehicle
excitation antenna is located at or near the base of the vehicle
body or radome where it has been found that the ionized layer
surrounding the re-entry vehicle during re-entry into the
atmosphere has a minimal affect on the antenna radiation
characteristics.
The various antenna constructions may be excited in a conventional
manner, i.e., the monopole of the embodiment of FIGS. 1-3 may be
excited in the conventional manner, the cavities 36 and 38 in the
embodiment of FIGS. 4 and 5 may be excited by a center probe or
loop, preferably in phase from a common source and the radome
antenna illustrated in FIGS. 6-8 may be excited with a post
extending across the cavity. The antenna constructions illustrated
excite currents on the skin of the vehicle body which flow along
the skin surface to produce a substantially constant radar cross
sectional area for the missile. A typical radiation pattern for an
antenna constructed in accordance with the present invention is
illustrated in FIG. 9 where a nose cone, generally indicated at 60,
is shown along a longitudinal axis 62 to provide a symmetrical
radiation pattern having a substantially symmetrical pair of lobes
64 and 66. The radiation pattern is plotted from the central point
68 with the relative power indicated along the vertical axis 70.
The zero db level is illustrated by the circle 72.
It should be understood that the invention is not limited to the
exact details of construction shown and described herein for
obvious modifications will occur to persons skilled in the art.
* * * * *