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    PARABOLOIDAL AND PROLATE-SPHEROIDAL IMPULSE RADIATING

    ANTENNAS WITH ILLUSTRATIVE EXAMPLES

    Dr. D. V. Giri

    Pro-Tech, 11-C Orchard Court, Alamo, CA 94507-1541 USA, [email protected], www.dvgiri.com

    ABSTRACT

    We start this paper with a four-band classification of

    high-power electromagnetic (HPEM) waveformsbased on bandwidth that has been recently proposed

    and formalized. An antenna system that radiates

    impulse-like waveforms making use of reflectors hasbeen called the impulse radiating antenna (IRA).

    More recently prolate-spheroidal surfaces are being

    considered to fabricate such antennas for specializedapplications. This paper presents these antennas along

    with some representative applications.

    1. INTRODUCTION

    It is well established that sufficiently intenseelectromagnetic (EM) signals in the frequency range

    of 200 MHz to 5 GHz can cause upset or damage in

    electronic systems. This induced effect in an

    electronic system is commonly referred to as

    intentional electro-magnetic interference (IEMI).Such an intentional electro-magnetic

    environment (IEME) can be:

    a single pulse with many cycles of a singlefrequency (an intense narrowband signal that

    may have some frequency agility),

    a burst containing many pulses, with eachpulse containing many cycles of a single

    frequency,

    an ultra-wideband pulse (spectral contentfrom 100s of MHz to several GHz), or

    a burst of many ultra-wideband transientpulses,

    Note that all of the above EM environments could be

    radiated or conducted. One way of classifying the

    HPEM environments is based on the frequency

    content of their spectral densities as narrowband,moderate band, ultra-moderate band and

    hyperband. To characterize these environments, we

    consider the bandratio of the EM spectrumas ( / )hbr f f = l . Using the inherent features of br

    in a manner consistent with the emerging EM field

    production technologies, the definitions forbandwidth classification presented in Table 1 has

    been proposed [1, 2].

    TABLE 1

    HPEM CLASSIFICATION BASED ON BANDWIDTH

    Band type

    Percent bandwidth

    1200 (%)

    1

    brpbw

    br

    =

    +

    Bandratio

    br

    Narrow< 1% < 1.01

    Moderate

    1%

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    2

    2. HYPERBAND SYSTEMS

    (163.64 % < pbw < 200%) or ( br> 10)

    Since it was the first proposed in 1989 [5] ,

    paraboloidal reflectors fed by TEM transmission lines

    have received a lot of attention, owing to their main

    attractive property of extremely wide bandwidth,

    without the adverse effects of dispersion. They havebeen called the impulse radiating antennas (IRAs) anda photograph of an example, the prototype IRA in

    Figure 1.

    Figure 1. Photograph of the 3.67m Prototype IRA

    The bandwidth associated with time-domain antennas

    is to be distinguished from the approximately 10 to 1

    bandwidth of the so called frequency independentantennas such as the log-periodic antenna, which is

    highly dispersive since the phase center of the

    antenna is not fixed. Different CW frequencies

    applied to a log-periodic antenna get radiated from

    different portions of the antenna, which makes itdispersive, if all of the frequencies are applied at the

    same time as in a pulsed application. Reflector IRAs

    overcome this problem and even have equivalentelectric and magnetic dipole moments characterizing

    the low-frequency performance. Even the dipolar

    radiation at low frequencies is along the optical axis

    of the reflector. Many optimal reflector IRAs hasbeen designed, fabricated and tested. Some of them

    are summarized in Table 2 with various performance

    parameters.

    3.ILLUSTRATIVE APPLICATIONS

    Hyperband systems can be built in many forms such

    as reflector IRAs described above, or TEM horns [6],

    and lens IRAs [7]. They have useful applications such

    as:

    Disrupter (Disrupting Integrated System,Releasing Ultra-PowerTransient

    Electromagnetic Radiation) [8]

    Buried target detection such as demining [9]

    Hostile target detection and identification[10]

    Space debris detection Periscope detection Source for vulnerability studies via transfer

    functions [11]

    high-power, hyper -wideband jammers [12] law-enforcement applications such as

    seeing through walls [13] Electrical characterization of materials (e.g.,

    wave propagation measurements inmaterials such as rock, concrete etc.,)

    Industrial applications (detection of leaky ordefective pipes) [14]

    Detection of human beings in earthquakerubble [15]

    Searching for avalanche victims [16] Artillery application [17]etc.

    They can be designed to operate from 10s of MHz toseveral GHz. This is an extremely wideband spectrum

    where critical military and civilian operations take

    place in the field of radar and communicationengineering.

    We will briefly discuss three of the above

    mentioned applications.

    3.1 Transfer Function of Buried Facilities

    The Swiss IRA described in Table 3 was employed in

    measuring the responses of a buried test-bed facility

    for HPEM environments. The facility was a concrete

    reinforced building buried in the earth. It had a smallabove-ground concrete structure that provided

    protection for the stairway leading from the surface to

    the working area below, as seen in figure 2.

    Figure 2. Exterior view of the underground Swisstest-bed facility

    The test data was gathered for both the pulse and CWilluminations. The same IRA was used for both types

    of excitations. Figure 3 represents the measuredtransient E-field from the IRA at a distance of 6 m

    from the radiator.

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    Table 2. Some examples of Paraboloidal reflector IRAs with performance characteristics

    0 2E-008 4E-008 6E-008 8E-008 1E-007

    Time (s)

    -400

    0

    400

    800

    1200

    E(t)(V/m)

    Data File M001.datd = 6 m

    Figure 3. Measured transient IRA field at a distance of 6m from the antenna

    # Name Pulser Antenna Far field r E r E / Vo br

    1 Prototype IRA

    AFRL, KAFB, NM USA

    + 60 kV

    100ps/20ns

    200 Hz

    3.66m dia

    (F/D) = 0.33

    4.2 kV/m

    at r =

    304m

    1280 kV 10.67 100

    2 Upgraded Prototype IRA

    AFRL,KAFB, NM, USA

    + ~ 75 kV

    85 ps/ 20 ns

    ~ 400 Hz

    1.83 m dia

    (F/D) = 0.33

    27.6 kV/m

    at r = 25 m

    690 kV 5 to 6

    (est.)

    50

    3 Swiss IRA, NEMP Lab,

    Spiez, Switzerland

    2.8 kV

    100 ps/4 ns

    800 Hz

    1.8 m dia

    (F/D) = 0.28

    220 V/m

    at r = 41 m

    10 kV 4 50

    4 TNO IRA

    The Netherlands

    9 kV

    100 ps/ 4 ns

    800 Hz

    0.9 m dia

    (F/D) = 0.37

    Not

    available

    34 kV 3 to 4 24

    5 Magdeburg, Germany 9 kV

    100 ps/ 4 ns

    800 Hz

    0.9 m dia

    (F/D) = 0.37

    Not

    available

    34 kV

    (est.)

    3 to 4

    (est.)

    24

    6 Pro-Tech, Alamo, CA 2.8 kV

    100 ps / 4 ns

    800 Hz

    23 cm dia

    (F/D) = 0.35

    Not

    available

    10 kV

    (est.)

    3

    (est.)

    6

    7 Pro-Tech, Alamo, CA Yet to be

    measured

    10 cm dia

    (F/D) = 0.33

    Not

    available

    Not

    available

    Not

    available

    2.6

    6

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    In this measurement, a number of different antenna

    locations and observation points for EM fields and

    induced wire currents were made. One of the first facility

    measurements made was with the IRA source located atthe main entrance. The measured transient and computed

    spectral E-fields inside the facility with the main dooropen and shut cases are illustrated in figure 4.

    At the bottom of the stairs in the facility entrance was

    a power system interconnection panel, where a groundwire was instrumented with a current probe.

    0 2E-008 4E-008 6E-008 8E-008 1E-007

    Time (s)

    -1000

    -500

    0

    500

    1000

    1500

    E(t)

    (V/m)

    Data File M006.dat

    M007.dat

    (door open and shut)Door open

    Door shut

    1E+007 1E+008 1E+009 1E+010

    Frequency (Hz)

    1E-011

    1E-010

    1E-009

    1E-008

    1E-007

    1E-006

    1E-005

    0.0001

    |E()|(V/m/Hz)

    Data File M006.datM007.dat

    (Door open and shut)

    Door openDoor shut

    Figure 4. Measured E-filed inside the facility with

    the door open and shut configuration

    Measured transient current in this wire is shown in

    Figure 5.

    Figure 5. Measured transient current on a power lineneutral and the corresponding computed

    spectral magnitude

    The testing of this buried facility resulted in a number

    of interesting results both for the EM field penetrationinto the facility, as well as for the induced currents in

    power and communication lines. From these

    measurements transfer functions are calculated and can

    be compared with computational models. With the IRA

    as a pulsed antenna, the transfer function measurements

    are done by a Fourier transformation of the inducedtransient responses, thus greatly reducing the problem

    complexity.

    3.1 JOLT (Hyperband Radiator)The JOLT antenna is a half-IRA with a 3.05m diameter,

    paraboloidal, commercial microwave reflector that has

    been cut in half and flanged for attachment to the ground

    plane. The transient energy source located at the focalpoint of this reflector launches a near-ideal TEM

    spherical wave on to the reflector through a

    polypropylene lens to be reflected as a collimated beam.

    A line schematic diagram and a photograph of the JOLT

    system are shown in figures 6 and 7.

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    Figure 6. Schematic of a Half IRA

    Figure 7. Photograph of JOLT Radiator

    The JOLT is a high-voltage transient system built at

    the Air Force Research Laboratory, Kirtland AFB, NM

    during 1997-1999. The pulsed power system centers on a

    very compact resonant transformer capable of generating

    over 1 MV at a pulse repetition frequency of 600 Hz.This is switched via an integrated transfer capacitor and

    an oil peaking switch onto an 85 Ohm half IRA. This

    unique system will deliver a far radiated field with a full-

    width half maximum (FWHM) on the order of 100 ps,and a field range product ( r E peak) of ~ 5.3 MV,

    exceeding all previously reported results. Arepresentative measured far-electric field is shown in

    Figure 8.

    Figure 8. Measured electric field at a boresight

    distance of r = 85m

    It is seen that the impulse-like radiated field from the

    JOLT seen in figure 8 has an extremely large bandwidth

    ranging from about 40 MHz to about 4 GHz or a band

    ratio of 100. Such HPEM environments are useful in

    specialized applications.

    3.2 Seeing Through Walls

    Tatoian et al [13] have employed a reflector IRA pair

    (transmit and receive) to get a one-dimensional through

    the wall radar signatures of certain objects. Figure 9presents a representative sample of the measured data.

    The shown signatures are the result of 2-way wave

    propagation (Impulse radar- generated wave propagatesthrough-the-wall scatters from the target on the other side

    of the wall, comes back through the same wall and is

    received by the same radar).

    Figure 9. One-dimensional through the wall radar

    return signal Man only (red)M16 only (blue) Man with

    M16 (black),

    The test wall consisted of an 8-inch concrete slab with

    two layers of 3-gage metallic rebar inside and yielded 56

    dB two-way power attenuation. The targets included

    Man, Man and M16 rifle, M16 rifle only. Each graph infigure 11represents true radar signature, or signal-related

    voltage, S, associated with the specific test target. The

    time axis corresponds to a round-trip travel distance of15.24 m. Work is in progress in this area and expected to

    lead to target imaging using Impulse Synthetic Aperture

    Radar (ISAR).

    4. Prolate-Spheroidal IRA

    Paraboloidal IRAs described above produce a beam thatis focused at infinity. There are emerging applicationsthat require focusing at a finite distance. This is possible

    if the reflector is a prolate spheroid instead of a

    paraboloid [18, 19, 20 and 21]. The prolate spheroid hastwo foci. The antenna is excited at one of the foci and the

    energy is focused at the second focal point.

    0 1 .108

    2 .108

    3 .108

    4 .108

    5 .108

    2

    1

    0

    1

    2

    3Through-the-Wall Sensing: Combined

    Time, sec

    Voltage,

    V

    2.36

    1.699

    ds1n

    ds2n

    ds3n

    4.995108.0 timen

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    6

    5.Summary

    In this paper, we have presented the 4-way classification

    of HPEM environments based on bandwidth. Thisclassification is based on emerging technologies and

    example systems in each of the four categories are alsodescribed. In addition, illustrative examples of

    Hyperband radiators, which are finding many useful

    applications both in the military and civilian sectors, are

    described.

    References1. D. V. Giri, Classification of Intentional

    Electromagnetic Interference (EMI) Based on

    Bandwidth, AMEREM 2002, Annapolis, Maryland,

    2-7 June 2002.

    2. D. V. Giri and F. M. Tesche, Classification ofIntentional Electromagnetic Environments (IEME),

    IEEE Transactions on Electromagnetic

    Compatibility, Volume 46, Number 3, August 2004.

    3. V. Fortov, F. Loborev, Yu. Parfenov, V. Sizranov,B. Yankovskii,, and W. Radasky, Estimation of

    Pulse Electromagnetic Disturbances Penetrating

    into Computers Through Building Power andEarthing Circuits, Metatech Corporation, Meta-R-

    176, December 2000.

    4. V. Fortov, Yu. Parfenov, L. Zdoukhov, ,R. Borisov,S. Petrov, L. Siniy, and W. Radasky,Experimental

    Data on Upsets or Failures of Electronic Systems toElectric Impulses Penetrating into Building Power

    and Earthing Nets, Metatech Corporation, Meta-R-

    187, December 2001.5. C. E. Baum,Radiation of Impulse-Like Transient

    Fields, Sensor and Simulation Note 321,

    November 25, 1989.

    6. C. E. Baum, Low-Frequency Compensated TEMHorn, Sensor and Simulation Note 377, 28 Jan 1995.

    7. E. G. Farr,Boresight Field of a Lens IRA, Sensor andSimulation Note 370, October 1994.

    8. C. E. Baum, The Disrupter, Transient Radiating

    Antenna Memo 4, 19 May 1998.

    9. Humanitarian Demining at TNO Laboratory, The

    Hague, The Netherlands.

    10. Detection and Identification of Visually ObscuredTargets, edited by C. E. Baum, published by Taylor

    and Francis, 1998.

    11. F. M. Tesche, D. V. Giri, P. F. Bertholet, A. Jaquier,and A. W. Kaelin, Measurements of High-Power

    Electromagnetic Field Interaction with a Buried

    Facility, ICEEA Torino, 10-14 September 2001, pp99-102,

    12. C. E. Baum, et. all.,JOLT: A Highly Directive, Very

    Intensive, Impulse-Like Radiator, Invited Paper in theProceedings of the IEEE, Special Issue on Pulsed

    Power Technology and Applications, pp 1096-1109,

    July 2004.

    13. J. T. Tatoian, D. V. Giri, R. Manzano, and G. Gibbs,

    Feasibility of an ImpulseRadiating Antenna (IRA) forThrough the Wall Sensing, ICEAA Torino, 8-12

    September 2003, pp 389-392.

    14. C. Maierhofer, T. Kind, J. Woestmann, and H.Wiggenhauser, Antenna Development for ImpulseRadar Applications in Civil Engineering, EUROEM

    2004, Magdeburg, Germany, 12-16 July 2004.

    15. I. Akiyama, Y. Araki, M. Isozaki, M. Ohki, and A.Ohya, UWB Radar System Sensing of Human Being

    Buried in Rubbles for Earthquake Disaster,EUROEM 2004, Magdeburg, Germany, 12-16 July

    2004.

    16. W. A. Chamma, H. Mende, and R. Robinson, UltraWideband Radar for the Search of AvalancheVictims, EUROEM 2004, Magdeburg, Germany,

    12-16 July 2004.

    17. H. Herlemann, M. Koch, and F. Sabath, UWBAntenna for Artillery Applications, EUROEM 2004,

    Magdeburg, Germany, 12-16 July 2004.18. K. Kim and W. R. Scott, Jr, Analysis of Impulse

    Radiating Antennas with Ellipsoidal Reflector,

    Sensor and Simulation Note 481, 31 October 200319. C. E. Baum, Producing Large Transient

    Electromagnetic Fields in a Small Region: An

    Electromagnetic Implosion, Sensor and Simulation

    Note 501, August 2005.

    20. C. E. Baum, Focal Waveform of a Prolate-Spheroidal IRA, Sensor and Simulation Note 509,

    February 2006

    21. D. V. Giri, Analysis of an Impulse RadiatingAntenna with a Prolate-Spheroidal Reflector,

    presented at the AMEREM 2006 Symposium held at

    Albuquerque Convention Center, July 10-14,

    Albuquerque, NM.

    1967 and 1969, respectively. He continued his graduate

    study at Harvard University receiving M.S. (Applied

    Mathematics, 1973) and Ph.D (Applied Physics, 1975).

    Dr. Giri has taught in the Dept. of EECS, University of

    California, Berkeley campus and is presently a self-

    employed consultant as Pro-Tech, in Alamo, CA, doingR&D work for U.S. Government and Industry. Dr. Giri

    was a Resident Research Associate for the National

    Research Council at the Air Force Research Laboratory(AFRL) Kirtland AFB, New Mexico, (1975-77). Dr. Giri

    is a senior member of the IEEE Society of Antennas andPropagation, a Charter member of the ElectromagneticsSociety, and Associate member of Commission B, URSI

    and member of Commission E, URSI. He has served as

    an Associate Editor for the IEEE Transactions onElectromagnetic Compatibility. He is an EMP Fellow of

    Summa Foundation in 1994 for his contribution to EMP

    simulator design HPM antenna design. He has published

    two books, one book chapter and over a hundred papers,

    reports etc. He is also a recipient of the John KrausAward from the IEEE for 2006.

    D. V. Giri was born in India and

    is a naturalized U.S. citizen. He

    received the B.Sc. degree in

    Physics and Mathematics fromMysore University in 1964. He

    then entered the Indian Institute of

    Science and received the B. E.

    and M. E. (Microwaves) in