GEOPHYSICS, VOL. 38, NO. 3 UUNE 1973), P. 557-580, 10 FIGS., 7 TABLES

RADIO INTERFEROMETRY DEPTH SOUNDING: PART I-THEORETICAL DlSCUSSlONt

A. P. ANNAN*

Radio interferometry is a technique for mea- layer earth. Approximate expressions for the fields suring in-situ electrical properties and for detect- have been found using both normal mode analysis ing subsurface changes in electrical properties of and the saddle-point method of integration. The geologic regions with very low electrical conduc- solutions yield a number of important results for tivity. Ice-covered terrestrial regions and the the radio interferometry depth-sounding method. lunar surface are typical environments where this The half-space solutions show that the interface method can be applied. The field strengths about modifies the directionality of the antenna. In a transmitting antenna placed on the surface of addition, a regular interference pattern is present such an environment exhibit interference maxima in the surface fields about the source. The intro- and minima which are characteristic of the sub- duction of a subsurface boundary modifies the surface electrical properties. surface fields with the interference pattern show- This paper (Part I) examines the theoretical ing a wide range of possible behaviors. These the- wave nature of the electromagnetic fields about oretical results provide a basis for interpreting various types of dipole sources placed on the sur- the experimental results described in Part II. face of a low-loss dielectric half-space and two-

INTRODUCTION lunar surface material has similar electrical prop- The stimulus for this work was the interest in erties. the measurement of lunar electrical properties in Since electromagnetic methods commonly used situ and the detection of subsurface layering, if in geophysics are designed for conductive earth any, by electromagnetic methods. Unlike most problems, a method of depth sounding in a dom- regions of the earth’s surface, which are conduc- inantly dielectric earth presented a very different tive largely due to the presence of water, the lunar problem. One possible method of detecting the surface is believed to be very dry and, therefore, presence of a boundary at depth in a dielectric is to have a very low electrical conductivity (Strang- the radio interferometry technique, first suggested way, 1969; Ward and Dey, 1971). Extensive ex- by Stern in 1927 (reported by Evans, 1963) as a perimental work on the electrical properties of method to measure the thickness of glaciers. The dry geologic materials by Saint-Amant and only reported application of the technique is the Strangway (1970) indicates that these materials work of El-Said (1956), who attempted to sound are low-loss dielectrics having dielectric constants the depth of the water table in the Egyptian des- in the range 3 to 15 and loss tangents considerably ert. Although he successfully measured some in- less than 1, in the Mhz frequency range. Analysis terference maxima and minima, his method of of the electrical properties of lunar samples by interpretation of the data is open to question in Katsube and Collett (1971) indicates that the light of the present work.

t Presented at the 39th Annual SEG International Meeting, September 18, 1969. Manuscript received by the Editor April 6, 1972; revised manuscript received September 22,1972. * University of Toronto, Toronto 181, Ontario, Canada. Downloaded 12/13/19 to 198.120.252.61. Redistribution subject SEG license or copyright; see Terms of Use at http://library.seg.org/ @ 1973 Society of Exploration Geophysicists. All right reserved.

557 558 Annan

The radio interferometry technique is concep- electrical properties of the earth and can be used tually quite simple. The essential features of the as a method of inferring the earth’s electrical method are illustrated in Figure 1. A radio-fre- properties at depth. quency source placed on the surface of a dielectric The problem chosen for study in the theoretical earth radiates energy both into the air (or free work was that of the wave nature of the fields space) above the earth and downward into the about various point-dipole sources placed on the earth. Any subsurface contrast in electrical prop- surface of a two-layer earth. The mathematical erties at depth will result in some energy being solution to this type of boundary-value problem reflected back to the surface. As a result, there is found in numerous references. The general will be interference maxima and minima in the problem of electromagnetic waves in stratified field strengths about the source due to waves media is extensively covered by Wait (1970), traveling different paths. The spatial positions of Brekhovskikh (1960), Budden (1961), Norton the maxima and minima are characteristic of the (1937), and Ott (1941, 1943). Although the solu-

Air Transmitter Receiver

Dielectric

(4

Transmittei-receiver separation (b) FIG. 1. (a) Transmitter-receiver configurationfor radio interferometry, showinga direct wave and a reflected Downloaded 12/13/19 to 198.120.252.61. Redistribution subject SEG license or copyright; see Terms of Use at http://library.seg.org/ wave. (b) Schematic sketch of typical field-strength maxima and minima as the transmitter-receiverseparation increases. Radio Interferometry: Part I 559

tion to the boundary-value problem can be found The geometry and coordinate systems used in analytically, the integral expressions for fields the boundary-value problem are shown in Figure cannot be evaluated exactly. In the radiation 2. A point-dipole source is located at a height h zone, approximate solutions to the integrals can on the z-axis above a two-layer earth, where the be obtained by use of the theory of complex vari- earth’s surface is in the x-y-plane at z = 0, and the ables and special methods of contour integration. subsurface boundary is at z= -d. The region The preceding references, plus numerous others, z>O is taken as air or free space. The region discuss these techniques in detail. Since much of -d

L

2 = h--~----~---~--_____ Sourct I 1 Region0 KO=MO=l

,

/- Region1 Kl, Ml X Z = -d\ 7

Region2 K2, M2

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This choice of scaling parameter makes all the vm + k?rI = - ; 1 (1) following integral solutions dimensionless. As shown by Sommerfeld (1909) for a half- with the electric and magnetic fields defined by space earth, and extended to a multilayered earth by Wait (1970), the Hertz vectors for the vertical E = Kzn + vv .I& (2) dipole sources have only a z-component, while for the horizontal dipole sources, the Hertz vectors and have both x- and z-components. The vertical di- H = - iwKe,,V X n (3) pole sources have solutions of the form where k is the propagation constant. wd/KMeopo n; = -@OR and eo,~0 denote the and permeabil- R ity of free space throughout. P is the electric di- pole moment density distribution. Similarly, for uo(X)e-Po(Z+h)H~(Xp)dX, (10) magnetic dipole sources, the results for the mag- m 0 netic Hertz vector are +kr ;

V2n + K2n = - M, (4) l-&L- * x [al@) ePIZ + a2(X)e-Prz] 2w s -_m PO and .e-PohZ3~(Xp)dX, (11) H = K2n + vv *II, (3) E = iwM/.o,v X II, (6) and

where M is the magnetic dipole moment density distribution. (12) The dipole sources are taken as “unit” point . eP*Z+(PZ-Pl)d-POh~~(~p)~~, dipole sources located in the region 220. The density distribution is X is the separation constant of the differential equation, and pj= (X2- ky)12,’ with the sign of the P = 4xei$(R)ej, (7) root being chosen such that the solution satisfies where ej is a unit vector in the z-direction for the radiation condition. In the above form, after a vertical electric dipole source and in the scaling by W, X is a dimensionless parameter, and x-direction for the horizontal dipole source. 6(R) kj= 2s(KjMj)12‘ is the relative propagation con- is the three-dimensional delta function, and stant of each region. The aj(X) are unknown func- R= [~2+y~+(z-k)2]12.’ Similarly for the mag- tions of X which are found by satisfying the netic dipole sources, boundary conditions that tangential E and H be continuous at z = 0 and z = -d. M = 4&(R)ej. (8) For horizontal dipole sources, the solutions for the Hertz vector take the form In the following discussions, no distinction be- tween the electric and magnetic Hertz vectors is eikoR made. When we refer to electric dipole sources, r( = - the electric Hertz vector is implied; for magnetic WR (13) dipole sources, the magnetic Hertz vector is im- plied. In addition, the free-space wavelength is bo(X)e-PO(Z+h)B~(Xp)dX, taken as the scaling parameter for all length mea- +iJ_-m G0 surements. In other words, a distance, denoted p, and is in free-space wavelengths, and the true length is Wp, where W is the free-space wavelength: cos+ - x2 n; = - COG9 2* 2w s-_m -PO (14) w= (9)

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for region 0; corresponds to setting both z and It equal to 0 in the preceding expressions for the Hertz vectors. nr, 2.2w _I; [bl(A)eP1z + b2(A)e-P1zl In the following discussions, h is always set equal s to 0, and, in most instances, z is assumed to be (15) close to 0. The solutions are discussed in two -e-PohH~(Xp)dX, parts; the half-space solutions and the two-layer and earth solutions. The half-space solutions for the Hertz vectors are obtained by setting KI= K2 and Ml= Mz in expressions (10) through (18). The half-space solution is of considerable interest since (16) the fields about the source show interference maxima and minima without a subsurface re- flector present. It also provides a base level for for region 1; and detection of reflections from depth.

APPROXIMATE SOLUTIONS

(17) Half-space earth . ePtZ+.(PtP1)&Poh~~(~~)~~, The solution of the half-space problem is treated by numerous authors, and the wave nature of the and fields is well defined. In the following discussions,

2 COSQ O” A2 the results of Ott (1941) and Brekhovskikh (1960) nz = - - c&d are followed quite closely, and detailed discussions 2w s -00 PO (18) of various aspects of the solutions can be found in these references. The wave nature of the fields about the source is illustrated in Figure 3. The for region 2. wavefronts denoted A and B are spherical waves The parameters X and Pi are the same as for the in the air and earth regions; wave C in the air is vertical dipole solutions, and the coefficients hi(X) an inhomogeneous wave, and wave D in the earth and ci(X) are found by satisfying the condition has numerous names, the most common being that tangential E and H be continuous at the head, flank, or lateral wave. Waves C and D exist boundaries. only in a limited spatial region, which is defined The boundary conditions for the Hertz vectors as those points whose position vectors make an and the resulting expressions for @j(X), bj(X), and angle greater than & with the z-axis. The angle QL~ Cj(X) are tabulated in Appendix A. The expres- is related to the critical angle of the boundary and sions for ai( bj(X), and Cj(X) are written in terms is defined in Appendix B. of the TE and TM Fresnel plane-wave reflection All the dipole sources exhibit the same wave and transmission coefficients. Using this notation, nature. To demonstrate how the waves are de- the similarity of all the solutions is clearly empha- rived from the integral expressions, the vertical sized and makes general discussion of the solu- magnetic dipole source is used for illustration. In tions possible rather than dealing with each source the air, the Hertz vector is given by separately. In discussing the approximate evaluation of the above integral expressions, extensive use is made II; = g + $J sin BoRoI(Bo) (19) of the plane-wave spectrum concept, since the e wave nature of the problem is most clearly under- .eikoz conB~H;(kop sin 8o)&o, stood using this approach. A brief outline of the .plane-wave spectrum notation used and approxi- and in the earth by mate evaluation of integrals by the saddle-point method is given in Appendix B. For radio interferometry applications, the fields at the earth’s surface for the source placed

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FIG. 3. Wavefronts about a dipole source on the surface of a half-space earth. A and B are spherical waves in the air and earth, respectively, wave C is an inhomogeneous wave in air, and D is the head wave in the earth.

With the aid of the Hankel transform identity and (Sommerfeld, 1949),

eikoR ik,, sin e. WR=iif s c (21) (24) .eikolzI coaeoI!Z~(kop sin &J&3,,, - GR[z%(a) + cot ar:a(41}, and the relation R,j= T,j- 1 for the Fresnel coeffi- 1 cients, equation (19) becomes where R= (p2+22)1/2, and a!= tan-l p/lZl . Ex- pressions (23) and (24) correspond to the spheri- cal waves A and B in Figure 3. The bracketed .eikolzI coSeoZY~(kOp sin Oo)dOo. terms on the right may be interpreted as the modification to the directionality of the source Using the saddle-point method as discussed in due to the presence of the boundary. Appendix B, the approximate solutions of the The waves C and D are generated by crossing integral expressions (20) and (22) are the branch points of ToI and Tlo to obtain the saddle-point solutions (23) and (24) for angles cr>a”. As outlined in Appendix B, the contribu- II; = tion of the branch point can be approximately (23) evaluated by the method of steepest descent as long as (Y is not close to the branch point. For (Y>cyc the expressions

2 21 2iklqoI(l - cot LYtan $,I)-3’2eik1P-(k1-ko) ’ I; = , (25) (k: - k;) Wp2

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2 21 2iko4 1 - cot a! tan ~EO)-32eikop--i’ k1--kg’ ’ ’ I; = (26) (k; - Ki) wp2

must be added to (23) and (24) in order that the der Waerden, 1951; Brekhovskikh, 1960; and solutions be correct. Expression (25) is readily Wait, 1970) have considered the problem since identified as the inhomogeneous wave C, and (26) then using the modified saddle-point technique to corresponds to the lateral wave D. evaluate the integrals for a*7r/2. While a true The asymptotic solutions have the form of the surface wave is not excited, the pole enhances the geometrical optics solution plus second-order cor- fields near the source in such a manner that they rection terms. For a perfectly dielectric earth, fall off approximately as (kR)-I. At large dis- expressions (24) and (26) become infinite as (Y tances from the source, the fields are those deter- approaches &. The singular behavior arises from mined by the normal saddle-point method which the second-order terms which depend on the have a (kR)+ fall off. The transition between the derivatives of T&Q. The first-order term which ranges is determined by the proximity of 8~ to is the geometrical optics solution remains x/2. In the radio interferometry application, the bounded. In this particular case, the angle (Ye earth properties of interest are those of a low-loss is the critical angle of Tl&). As a result, the sad- dielectric which is assumed to have only moderate dle point and branch point coincide at a=&, and contrasts with the free-space properties. The pole the approximate methods used to evaluate the in this case is well away from x/2 and does not integrals are no longer valid. The conical surface affect the preceding solutions. about the z-axis, defined by (Y=o!, is the region In the particular situation of an earth where where the lateral and spherical waves merge to- MO= Ml, the Hertz vector for a vertical magnetic gether. In this region the two waves cannot be dipole can be evaluated exactly for z=h=O. The considered separately; the combined effect of the result is saddle point and branch point must be evaluated. Detailed analysis of this region for integrals sim- &&-- 2 [eik+ko-;) (27) ilar to expression (20) is given by Brekhovskikh (kf - ki) wp2 (1960), who obtains an asymptotic solution with 1 the geometrical optics solution, as the leading _eiklp &__ , term plus a connection term which falls off as ( P (k,R)+4 instead of (k1R)-2. This result indicates )I that the geometrical optics solution still describes as shown by Wait (1951). This provides a check the fields adequately for a=& when (klR)+14<

tions is to equate the radiation pattern of the source on the boundary to the first-order term in the preceding solutions. This technique demon- strates how the boundary modifies the directional- The Gi(a) for the various sources are tabulated in ity of the source. The radiation pattern is sharply Table 1. The electric and magnetic fields can be peaked in the direction of the critical angle into obtained by differentiation of the preceding solu- the earth. A sketch of the radiation pattern for a tions; the particular form of the integrals encoun- vertical dipole source is shown in Figure 4. This tered permits interchange of the integration and directionality of the source is important when re- differentiation steps. flections from a subsurface boundary are con- The half-space solutions demonstrated that sidered. interference patterns will be observed in the field strengths even when there is no subsurface re- Two-layer earfh flector. This is readily seen from equation (28). The fields at the earth’s surface are composed of The analysis of the integral expressions for the two propagating components with one having the two-layer eart?hproblem is carried out in two dif- phase velocity of the air, and the other the veloc- ferent ways. The depth of the subsurface boun- ity of the earth. Another important feature of the dary and the electromagnetic losses of the first half-space solutions is that the fields near the layer determine which approach is more useful. boundary fall off as the inverse square of the radial The primary method of analysis is to treat the distance from the source at distances greater than first layer of the earth as a leaky waveguide and two or three wavelengths from the source. use normal mode analysis. In certain cases the A convenient method of interpreting the solu- mode analysis is cumbersome, and these cases

Table 1. Coefficients G&Y) for half-space earth solutions for various dipole sources.

Hertz G2 Source Vector 1z G I I - ToI - i(G:(a)‘ + c:(a) cota) kf - k: - - Vertical Electric Sot(a) -i(G:'(a) + G:(a) cota) Dipole

Magnetic0 0 2ik&o, SOlb) -i(G:'(a) + G:(a) cota) Horizontal nx k; - k: Magnetic -- Dipole Magnetic0 1 (yo, - l)Tol(a)Solb) =&o‘ + mo) -i(G:‘(a) + 3G:(4 cot OJ- 2(&(m)) IIZ PPo(4 k;(kz0 - kz)“*I - Electric 0 0 -i(G:‘(a) + G&Y) cot a) Horizontal ax Electric - 2 2iko(mo + Em) -i(G:‘(a) + 3G:(a) cot a - 2G,(4) k;(kz0 - k:)lz

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FIG. 4. Sketch showinghow a dielectric boundary modifiesthe directionality of a vertical dipole sourceplaced on the boundary. (a) No boundary present. (b) Boundary at Z=O.

yield more useful results when the integrals are ik? solved approximately using the saddle-point II; = cos f#JG sin2 ~:m~~(Bdc~(fh) s c (31) method of integration. 1 The various dipole sources may all be treated in the same manner. For the purpose of illustrat- where the integration variable is &, as defined in ing the method of analysis, the horizontal electric Appendix B. The singularities of the coefficients dipole source solutions are used as an example. bo and COdetermine the nature of the solutions to The X- and z-components of the electric Hertz equations (30) and (31). vector in the air for this source are given by equa- The expressions tions (13) and (14) where the coefficients bo and GO are listed in Table A-2. rllO~lO(l+ R12P) For normal mode analysis, equation (13) is re- rnlO(l+ bo)= , (32) written using the integral identity [equation (21)]. 1 - R,oJW The components of the Hertz vector are given by and

1 d = 2 J sin4mlo(e1) [1 + bo(eI)](30) mlOcO= - C 2PO 1 . e&o2 coSeOHo(kIp sin OI)dO1, . (YOI- l)rlloTlo(l+R12~)So1(1+X1~B) Downloaded 12/13/19 to 198.120.252.61. Redistribution subject SEG license or copyright; see Terms of Use at http://library.seg.org/ and (1--~10X128)(1-R10R12B) 566 Annan

(1 - R1oRd3) = 2 (R1oRd3>“. (36) (l-xXlOX12P)(l-R1OR12P) _I --I‘ IL-0

have branch points at the two critical angles of The positions of the poles and branch points in the two boundaries in question. In addition, the complex plane determine the wave nature of equation (32) has an infinite set of simple poles, the solutions to equations (30) and (31). The nor- and (33) has a doubly infinite set of poles on each mal mode solutions are obtained by deforming the Riemann surface. These poles are determined by contour of integration C to C’, as schematically the normal mode equations, illustrated in Figure 5. The integral from -(r/2) +ia, tor/2+im, andfromr/2+im to 7r/2--im 1 - RroRizP = 0, (34) is identically zero. Along the first part of C’ the integral is zero since the integrand is zero. Along and the second part of the contour C’ the integral is 1 - x,ox,zp = 0. (35) zero due to the asymmetry of the integrand about &=x/2. This result is common in mode analysis Equations (34) and (35) are the TE and TM nor- and has a wide range of applications as discussed mal mode equations, respectively. Both are trans- in detail by Brekhovskikh (1960). The integral cendental equations with infinite sets of roots. The along C is equal to the residues of the poles crossed relation between the normal modes and multiple in deforming the contour to C’, plus the integrals reflections is readily obtained by expanding the along contours Cr and Cz which run from +im denominators of equations (32) and (33) into around the branch points and back to +im. The infinite geoi ric series. For example, components of the Hertz vector are given by

‘2 In i n/2 _- 1

I2 Ia3

FIG. 5. Complex&plane showinghow integration contour C is modified to C’ in order to obtain normal mode solutions.Branch points denoted by solid circlesand the poles by squares. Downloaded 12/13/19 to 198.120.252.61. Redistribution subject SEG license or copyright; see Terms of Use at http://library.seg.org/ Radio Interferometry: Part I 567

Table 2. Residues of Roles for normal mode analysis for horizontal electric dipole.

TE Mode Residue

0 IIZ TM Mode Residue

where t(&) = s o : [d-lo(eP)[i+ R,~cePh9CeP)]sdl+ xIr(ef)8(e3)l

lTi = 2zri c (TE pole residues) The solutions (37) and (38) are completely gen- (37) eral and valid provided a branch point and a pole, + 11 + 12, or a TE and TM pole, do not coincide. In the first and situation, the pole and branch-point contributions II: = 2ai c (TE pole residues) must be considered together rather than sepa- rately, as indicated. In the other situation, (38) + 27ri c (TM pole residues) (38) must include the residue of a second-order pole rather than the residues of two simple poles, as + Ia + 14, indicated. Since these situations rarely occur, they where are not discussed further here. The expressions for the residues in (37) and (38) are tabulated in Table 2. Approximate solu- tions to the branch cut integrals may be obtained by steepest-descent integration as discussed in Appendix B. The solutions are the second-order lateral and inhomogeneous waves generated at the I2 2$ sinem10(f4>[l + hml boundaries. The approximate solutions are listed . c2 (40) s in Table 3. . eaoz O”ne ”H&p sin el)del, The behavior of the fields at the earth’s surface . 2 is very dependent on the position of the singular points in the complex & plane, which points are, la = cos f#J 2 sin2el~lo(fh)431) (41) in turn, determined by the material properties of S Cl the earth and the layer thickness d. The important features of the solutions are the radial depen- dences and the initial amplitudes of the various . 2 terms in the solutions. All the residues contain 14 = cos#j”k’ Hankel functions, which, for radial distances 2w Sc* sin2 ~l~lo(~l)dv (42) 1 greater than one or two wavelengths, have the . eikoZcon eoHI(klp sin el)d81. form Downloaded 12/13/19 to 198.120.252.61. Redistribution subject SEG license or copyright; see Terms of Use at http://library.seg.org/ 568 Annan

Table 3. Approximate steepest-descent solutions to branch-cut integrals for normal mode analysis of the horizontal electric dipole.

2 2 ikg 2ikos,a(l + R12(&)8(dO)) e (k: - ki)(l - R1*(@$8(~iJ)*WP*

I (1 _ COt (ydtan e;,)- Ji2Ca(eEe)ek0p+i2d(k:--k~)1a’ cos +ko Cl(e;O)elkop -_ 2(k:-_ 0 WP2 WP2 1

* * “22d-(k;-k;)l~z’ cos qkr(l - cot LYEtan 0&)-a/2C3(8~;)k ’zP--(kZdL) 2(k: - k;)“Wp”‘

7jOl(l - I&)(1‘ + XI& ’ + Eo,(l - x:*8*)(1 + iWqz cl(eL) - (1 - xl*s)*(l - RlZS) ’ 1

c,(ekd

2iqloTloS01&T{ (701 - l)[.&S~o(l + To@ - Ru@) + t112T10(1+ SoIS - X~@)l 2(1 - y&o1y&z1(l + X&(l - RIO@)+ vz1(1 - x~~6)(1 + R&l) cde2 - - kr,(l - yz~)l”(l - yz~)“~(l - X&)(l‘ - &S)*

ko kz sin eEo= - sin eEz= - h k1

--Illeiklp sin BP1 with Kt< K1 in case (c). In all cases MO= Ml= Mt P , (43) is assumed since permeabilities of bulk earth ma- where @ is a pole defined by equations (34) and terials vary little from the free-space value. The (35). The branch cut contributions, II and 13, poles lie on the lines 1I&&@[ = 1 and 1XIOX&I fall off as pe2 with no exponential attenuation, = 1, with the density of distribution of the poles while 12 and Z4 fall off as pe2and are exponentially on these lines controlled by the slab thickness d. attenuated when the earth is lossy. The ampli- For d small, the poles are widely spaced with most tudes of the modes are largest for those poles in of them lying high up the lines near the imaginary the vicinity of f?& This effect is related to the O1axis. For increasing d, the poles move down the modified directionality of the source as discussed lines toward &=r/2 and are more closely packed. for the half-space fields. When the earth has a Unattenuated modes occur only when the Oy lie finite loss all terms in the solution except II and on or close to the real O1axis. In case (a), the pole the first term of 13 have amplitudes which decay contours lie on the real axis for &, IO1

Downloaded 12/13/19 to 198.120.252.61. Redistribution subject SEG license or copyright; see Terms of Use at http://library.seg.org/ with Kz>K, in case (b), and a perfect dielectric damped due to energy leaking out of the slab. In Ko= 1 FREE SPACE

K* PERFECT DIELECTRIC

PERFECT CONDUCTOR

(4 Is 0.

Kg = 1 FREE SPACE

PERFECT DIELECTRIC -Re e1 K, n/2

K2 ’ K1 PERFECT DIELECTRIC

04 Im 8,

K, = 1 FREE SPACE

PERFECT DIELECTRLC /2Re 81 KI K2< K1 PERFECT DIELECTRIC

(4 FIG. 6. Sketches of complex Or-plane showing positions of branch points and pole lines for 3 simple two-layer earth cases; case (a), dielectric slab over a perfect conductor; case (b), dielectric slab over dielectric half-space with Kz>Kl; case (c) dielectric slab over a dielectric half-space with K*

case (b), no unattenuated mode can exist, since The Hertz vector components can then be writ- energy is continually flowing out of the slab into ten as the lower half-space. The effect of a finite loss ‘in the slab moves the pole contours up away from II: = JG+ Lx, (49) the real axis, and all modes have a finite attenua- and tion. These models demonstrate the general posi- tion and behavior of the singular points in the IC = La + L, (50) complex plane. More detailed studies are given by Wait (1970), Brekhovskikh (1960), and Bud- where L1 and La are the half-space earth solutions den (1961). discussed earlier, and L2 and L4, given by The normal mode approach is most useful when the distance from the source is greater than the depth of the boundary d and when the earth has a very low loss. In a lossy dielectric, the complex (51) dielectric constant is R’(l+i tan S), where K’ is 1 the real dielectric constant and tan 6 is the loss tangent; and the attenuation distance in free- and space wavelengths for a plane wave is

D= _!_ (44) q//K’ tan6’

when tan 6<1. When d approaches the attenua- aeitoz co8eo@Z1(K1p sin el)del tion distance, the solutions begin to approach describe the effect of the subsurface boundary. those of a lossy dielectric half-space. An alternate and can be approximately evaluated by approach to evaluating the fields when the dis- L2 LI the saddle-point method, which results in the ge- tance from the source is less than d, or when d 1 D, is desirable, since the normal mode approach is ometric optics solution. Since s is assumed close to zero throughout, the expression cumbersome in these cases. The integrals can be approximately evaluated by the saddle-point method of integration when B&RN sin 0,) (53) multiple reflections are not strong. The fields can then be expressed as the half-space solution plus in the integrands may be regrouped using the a contribution from the subsurface boundary. By asymptotic expansion of the Hankel function in regrouping the coefficients bo and COin the form the manner discussed in Appendix B. L2 and Lp then contain the expression bo = ROl + a;& (45) ,+2kld cm bl+ikip sin 81 = ,+lRd oos(dl-a.+) (54) SolTo co = f (701- 1) T + c$, (46) in the integrand, where Rd= (p2+4d*)1/2 and 0 ad= tan’-’ C9/2d). In this form cydis the saddle

TolTloR12 point of the integrand and is the geometric optics b: = (47) direction of a ray reflected from the subsurface (1 - RIO&@) ’ boundary. The saddle-point solutions of L2 and and LI, outlined in Appendix B, are

1 1 (YOI - ~)SOJOI[TIORI~’ + S1oX12 + (SOI + TOI - S~IT,,I)X~~R&] co =;i;;(; (1 - R10&28)(1 - X10X128) (48) _ (721 - l)S1~~loSlzmolTolylzTlz Downloaded 12/13/19 to 198.120.252.61. Redistribution subject SEG license or copyright; see Terms of Use at http://library.seg.org/ (I - &o&28)(1 - XloXd) 1* Radio Interferometry: Part I 571

Expressions (55) and (56) can be interpreted as P((Yd)- 2% (P”(CYd) having replaced the subsurface boundary by an 1 d image source at twice the depth. The image source -I (55) has a radiation pattern which depends on the re- + p((Yd)’ cot ad) , flection and transmission coefficients of the boun- I daries and the layer thickness. and In obtaining the saddle-point solution, the ef-

&klRd fect of the poles and branch points has been

L4 = cosdsinad- neglected; such neglect is justified when the WRd boundary is deep and the earth has a significant loss. This is illustrated in Figure 7. To obtain the * Q(%i)- & (Q”(w) (56) saddle-point contribution, the integration contour C must be deformed into the saddle-point contour I. The position of I in the complex 0, plane is + 3 cot adQ(ad)’ - 2Q((Yd)) , determined by ffd, which, in turn, is determined by 1 the ratio of the radial distance to the depth of the where boundary, p/2d. In order that a given pole or 1 branch point be crossed when C is deformed to I’, l/Z, P = mlo(CYd)bO((Yd)eikoZ(1--710sina ad) (57) ffd must exceed a certain value which is deter- mined by equation (B-11), which defines the con- and tour I. Since p=2d tan (Y,& the radial distance 1 Q = mlo(crd)co(~d)ekoZ(l-r~o’ sin ’ ad)“a. (58) from the source at which the singular point is

FIG. 7. Complex &-plane showing deformation of contour C to saddle-pointcontour r. Solid circles= branch points, squares= TE poles, and open circles= TM poles. Downloaded 12/13/19 to 198.120.252.61. Redistribution subject SEG license or copyright; see Terms of Use at http://library.seg.org/ 572 Annan

crossed in obtaining P is defined. When the singu- are generally few in number. Since each lar point is a pole, the contribution to the integral propagates radially with a different phase after crossing the pole is a residue of a form similar velocity, the fields will show a regular pe- to those in Table 2. When the pole is not on the riodic beating as the various modes move in- real 01axis, the residue is exponentially attenuated and out-of-phase. with increasing radial distance. The value of p at 3. When the first layer of the earth is lossy which the pole must be considered in determining and several wavelengths deep, the geometric the integral is also defined, and is usually much optics solution is more useful than the normal greater than the attenuation distance of the mode. mode approach. The expression for the fields As a result, the residue of the pole is extremely is the half-space solution plus a contribution small and is negligible compared to the saddle- from the reflecting boundary. This is the type point contribution. For cases when some poles lie of solution used by El-Said (1956). In El- on or near the real 81 axis, a fixed radial distance Said’s analysis, the waves propagating along from the source must be exceeded before their ef- the surface were not correctly expressed, and fect needs to be considered. Beyond this distance, the modification in directionality of the the normal mode approach is more convenient for source due to the air-earth interface was not expressing the solutions. considered. This form of solution is particu- The branch-point contributions yield inhomo- larly useful for a quick computation of the geneous and lateral waves generated at or reflected strength of reflections from subsurface from the subsurface boundary. As in the case boundaries and of the effect on surface fields of the poles, a finite distance from the source must of changes in electrical properties. be exceeded before these contributions need to be 4. The saddle-point solution is useful for considered. For the earth models where the saddle- determining the radial distance from the point method is useful, these contributions, which source at which the various contributions of are second-order effects, are negligible. When the singularities of the integrand become im- these second-order waves are significant in the portant. Since the saddle-point contour is determination of the field strengths at the earth’s positioned in the complex plane by the ratio surface, the normal mode approach is the better p/2d, a ratio p/2d can be defined for each method for computing the fields. singularity. For normal modes, the radial The two-layer earth solutions cover a wide distance defined by this ratio may be inter- range of possible responses. The important results preted as the distance from the source re- are as follows: quired for a given mode to develop. For the branch points, this ratio defines the critical 1. When the first layer of the earth is very distances from the source, where lateral thin and the second layer is a low-loss me- waves and inhomogeneous waves from the dium, the first layer is undetectable. The re- subsurface boundary reach the surface. sponse of the earth is the same as that of a half-space composed of the second layer of DISCUSSION the earth. The radio interferometry technique provides a 2. When the first layer of the earth is on method of determining electrical properties in the order of one wavelength thick, the sur- situ and of detecting subsurface stratification of face fields become extremely complex. The the electrical properties in environments which fields exhibit a p-r’* fall-off out to the attenua- are moderately transparent to electromagnetic tion distance of the least attenuated mode waves. The theoretical analysis of the two-layer which is strongly excited. Beyond this dis- earth problem defines the behavior of the fields at tance, the contribution of the modes becomes the earth’s surface and provides a basis for under- negligible and the second-order lateral and standing experimental results reported by Ros- inhomogeneous waves, with no radial ex- siter et al (1973) in Part II. The various solutions ponential attenuation, determine the field derived here are also useful for computing rough strengths which then fall off as p-z. When estimates of the interference patterns in the fields modes with low attenuation are excited, they at the earth’s surface, provided the asymptotic Downloaded 12/13/19 to 198.120.252.61. Redistribution subject SEG license or copyright; see Terms of Use at http://library.seg.org/ Radio Intevferometry: Part I 573

nature of the expressions is given due respect. useful unit of length when discussing and plotting Examples of these are given in Part II. radio interferometry data. Scale model construc- The half-space solutions provide a method of tion is based on keeping all dimensions the same determining the electrical properties for a half- on the wavelength scale and having the same loss space. Any strong departures from the half-space tangent. In the analysis of field data, plotting wave nature (i.e., a regular interference pattern distances on a wavelength scale makes compari- and a pe2 distance dependence) indicate that re- son of data taken at different frequencies straight- flections from depth are important. When the forward. If the electrical properties are not fre- reflections from depth are due to a horizontal quency dependent, running the experiment using boundary in electrical properties, the behavior of several different frequencies can effectively vary the fields varies considerably. For example, when the depth of a subsurface interface from a fraction normal modes are excited, the fields fall off as of a wavelength to many wavelengths. pw112with regular beating in the field strengths with distance from the source. APPENDIX A: COEFFICIENTS AND PARAMETERS The treatment of a two-layer earth with plane The coefficients in the integral expressions for boundaries, homogeneous media, and point the Hertz vectors for the various dipole sources sources is a considerable simplification of most are obtained by satisfying the boundary condi- real environments. These simple models and the tions at z=O and z= -d. Without a consistent approximate solutions obtained do, however, pro- notation, the coefficients are extremely compli- vide insight into the field behavior in the radio cated expressions, which lose the symmetry of interferometry application. Methods to accurately equations (1) through (6) and are difficult to compute field strengths for these models are cur- interpret physically. In this section, the solutions rently under investigation. The effect of rough for the coefficients are tabulated, and the notation and dipping boundaries on the solutions is ex- used throughout the body of the text is defined. tremely important. Also, the presence of scatter- In Table A-l, the boundary conditions for the ing by inhomogeneities in the earth can drasti- Hertz vectors are listed. In Table A-2, the expres- cally alter the fields at the earth’s surface. These sions for the ai( bj(X), and cj(X) are listed for problems are virtually impossible to treat in a each dipole source. Examination of these solutions general manner theoretically. Scale model experi- shows the symmetry between the electric and ments seem to be the most feasible method of magnetic dipole sources. Interchanging the roles studying these problems. This work is presently of Ki and Mi, one can readily obtain the solution in progress. for a magnetic dipole source from that of an The free-space wavelength provides the most equivalent electric dipole source, and vice versa.

Table A-l. Boundary conditions for Hertz vectors for various dipole sources.

Vertical Magnetic Dipole an; a&’ Magnetic _=__ (VMD) az az

Vertical Electric Dipole ad a&' Electric ZLII: = Ki+&l -=- NED) az az

Horizontal Magnetic Dipole Magnetic @MD)

K,I& = Kit&+ Horizontal Electric Dipole aIIi+l Electric (HED) Ki as = KitI ~ az Downloaded 12/13/19 to 198.120.252.61. Redistribution subject SEG license or copyright; see Terms of Use at http://library.seg.org/ 574 Annan

Table A-Z(a). Coefficients a<(h), hi(k), and c&x) much more apparent when the plane-wave for vertical dipole source. spectrum notation is used. The form of the plane- wave spectrum used throughout is obtained by Two-layer earth Half-space defining three complex angles, BO,&, 82,and trans- forming the integration variable by setting &I + RllS a0 ROl 1 - &d&4 X = k. sin B0 = K1 sin & = kz sin &. (B-l) -

Vertical al The angle 00 is used in the region 220, B1in the region -d 0 on the earth’s surface at an angle & to the z-axis is refracted into medium 1 at an angle &, aolTot?7lzTl* and to the z-axis and into medium 2 at an angle a3 rloJol 1 - R1oR128 02, as illustrated in Figure B-l. The reader is - referred to Clemmow (1966) for details. The expressions for the Hertz vectors in equa- x01 + x128 a0 X01 tions (10) through (18) transform as follows, 1 - X10X128 where the II”, for a vertical dipole has been chosen as an example: EOlSOl Vertical al EOlSOl 1 - x10x128 Electric II; = s + $ J sin eoao(eo) (B_2) c EOlSOlXlzS ___- Dipole a2 0 1 1 - xloxlzB - eikoCoIJ eo(Z+h)EZO(kOp sin e&e,.

E01S01E1zS12 The integration contour C runs from -5r/2+Ztoo a3 ~olsol 1 - XlOX12B to --a/2 along the real 00 axis to r/2 and then to 7r/2- im, as illustrated in Figure B-2. For the angles Bi, the contour C is obtained from equation The various parameters used in the solutions are (B-l). The Pi transform to -iki cos&, where the listed in Table A-3. negative sign is chosen in order to satisfy the radi- The expressions Xii, Sij, Rtj, and Tij are the ation condition. Substituting for P, in the Fresnel Fresnel plane-wave reflection and transmission coefficients of Table A-3 results in the more fa- coefficients. The subscript notation ;j has the fol- miliar form lowing meaning: subscript i denotes the medium from which the plane wave is incident on the plane ($-)“cos&-‘ cos ej boundary between media i and j. For example, the ($y” subscripts 01 mean a plane-wave incident from Xij= the air on the boundary between the air and the ($)l” cos ei+ (2)“’ cos first layer of the earth. The Xij and Sij are the e, ’(B-3) reflection and transmission coefficients respec- tively for a TM plane wave; the Rij and Sij are where the TM reflection coefficient is shown as the reflection and transmission coefficients for a an example. TE plane wave. The integral expressions can be approximately evaluated by manipulating the integration con- APPENDIX B: PLANE-WAVE SPECTRUM AND tour C in the complex 8 plane. The approach is to EVALUATION OF INTEGRALS replace the Hankel function by its asymptotic The physical meaning of the integral expres- expansion, which is valid when the argument is sions for the various Hertz vector solutions is considerably greater than unity. Downloaded 12/13/19 to 198.120.252.61. Redistribution subject SEG license or copyright; see Terms of Use at http://library.seg.org/ Table A-Z(b). Coefficients ai(x), b;(x), and G(X) for horizontal dipole sources.

Two-layer earth Half-space - Xa1fX1nS bo X01 1 -x10x128

Y&1 bl YOlSOl 1 -X1&128 --

0 -- YO&llYlzSl2 HMD ba YOlSOl 1 -x,0x126 --

-_

1 (yo,- l)&-o&(l+XlzB) - (m- 1MlO~l2mO1~olrl2Slz - Cl 2PO (1 --IZ&*8)(1 --x10x12i3 --

1 (m- l)?O,~,,~l2asO,~l+r,2~~ - ~r2l-~~~~2molro~Solrl2S~d 62 - 0 2PO (l-RlOR,*B)(1-xXloXl28) -- *

==

~o,Tol --

bz 0 --

HED ba YOJlll --

1 (yol- 1)&,&J-0,(1+&a) - (YZI- 1~Sl2X~o~o,rO~~ol~~2T128 -c_ (Yol-l)SO*Sol 2PO (l-Rl&28)(1-X10X12B) &0

1 (~~1-1)E01S01X128(1+R128)T01- (~21-1)S12m01~01T01~12T12B c2 - 0 2po (1--~10R128)(1-X10X12B) _ --

1 (YOI- l)~oS,lE,S,2T,,(l+R,zB) - (WI- 1)512S112(1+yO~~)mO~yO1~~1~12T,2 Downloaded 12/13/19 to 198.120.252.61. Redistribution subject SEG license or copyright; see Terms of Use at http://library.seg.org/ ca -- 2PO (l-RlaR12a)(l-XlOX12S) Table A-3. Parameters wed and Fresnel coefficients REGION 0 Parameters

k;

yij = ? Pi REGION 1 fl B @W mij = E Mi ki a KiMi(2r) ’ ?ij =Mi

TM Fresnel Coefficients X,, KjPi - KcPj Reflection: ” * KjPi + KiPj FIG. B-l. Illustration of integration variables 61,81, 2KjPi and & and Sell’s law. Transmission: Sij = KjPi + KiP, Relations: xij = - xji Xij a Sij - 1

Xij p 1 - Sfi sit 31 tisji mii (B-4)

TE Fresnel coefficients R,, MjPi- MiPj Reflection: and ” = MjPi + MiPj 2MjPi Transmission: Tij = MjPi f MiPj

Relations: Rij = - R,i Rij 0 Tij - 1 (B-5)

_ ?ii Tji Rij = 1 - Tji Tij w

FIG. B-2. ComplexB-plane showing contour C, saddle-pointcontours r and r’, and the positionsof the branch point

Downloaded 12/13/19 to 198.120.252.61. Redistribution subject SEG license or copyright; see Terms of Use at http://library.seg.org/ 8~and branch cut (chain line). Radio Interferometry: Part I 577

Substitution into the integrals, such as that in sin2 eA(e) equation (B-2), results in an expression of the S e (B-13) form .eikz co:o8eH:(kp sin 0)&. eiZk cm B+ikp ain 9 03-a The solutions to the second order are given by in the integrand, which can be written as

(B-7)

where R= @+Z*)**,‘ and R and (Y are just the (B-14) length and direction of the geometric-optics ray- path. An integral with exponential of the form (B-7) is amenable to the saddle-point method integration, where 19=a is the saddle point. By and deforming C to the contour of most rapid descent away from the saddle point r one obtains an 123r:- ik sin (Y asymptotic series in the parameter (kR)- ’ for the integral. The leading term in the series is the (B-15) geometric-optics solution to the problem. A”(cr)+3cotcuA’(cr)-2A(cr) . The saddle-point contour r is defined from the II argument of the exponential in expression (B-7). Along the contour r, Solutions (B-14) and (B-15) are valid as long as A (0) is a slowly varying function of 0 near the ikR cos (0 - a) = ikR - kR?, (B-8) saddle point cr. This assumption is valid provided A (0) does not have a singular point near Q. In the where expressions for the various A (0) appearing in the s2 = - sin (0’ - cr) sinh 0”, (B-9) text, branch points and poles of A (0) are of the utmost importance in the solutions. The branch and points of A (0) are the critical angles of the 8 = 8’ + ie”, (B-10) boundaries in the problem. The critical angles enter all the A(8) through the relation The contour r is then given by the equation COS Oj = f [l - yij sin* ei]*lz (B-16) cos (f3’ - CX)sinh 0” = 1 (B-11) in all the Fresnel coefficients subscripted ;j. and is illustrated in Figure B-2. The radical splits the complex e-plane into two An excellent evaluation of the particular types Riemann sheets with branch points at of integrals that appear in the text is given by Brekhovskikh (1960), and the reader is referred h sin& = f -. (B-17) to this reference for more detailed discussion. In ki the rest of the discussion, solutions to the integrals valid to the second order in kR_r are used. This For the two-layer earth there are two boundaries involves using the second-order terms in the which give two critical angles and result in a four- Hankel-function expansion and then taking the sheeted e-plane. In the half-space earth problem, asymptdtic solution to the integrals to the second the complex &plane is two-sheeted. The conven- order. The integrals in the text have two forms: tion followed throughout is that of taking the positive square root. The surface defined in this manner is referred to as the upper Riemann sur- sin eA(e> face. For one to evaluate the integrals, the branch (B-12) cuts from the branch points must be defined. The convention used here is the same as that of Ott .eikz co8 sin @de,

Downloaded 12/13/19 to 198.120.252.61. Redistribution subject SEG license or copyright; see Terms of Use at http://library.seg.org/ eI&kp and Brekhovskikh, who define the branch lines as and those contours along which the imaginary part of 578 Annan

equation (B-16) is zero. The branch line is the (n+l) iki chain line in Figure B-2. rg = ~ sinn+l &A (OJ (B_20) The branch points must be taken into account 2w sB for saddle-point angles greater than oc. As illus- trated in Figure B-2, for a>&, in order to deform .eikiz co8iHt(kip‘ sin Bi)dBi, contour C into r, the branch point 0” must be where the contour B runs from im to 0” on the crossed. A modified integration contour to take left of the branch cut and from 0” back to in 8” into account is shown in Figure B-3. As long as along the right of the branch cut. For approxi- cy and 8” are well separated, the saddle-point and mate evaluation, 1~ is rewritten branch-point contributions can be evaluated separately. The contribution of the branch point n+l iki 1/Z is a second-order effect (Ott, 1941) as long as IgIv-- cr#B” and an approximate evaluation of the 2w e- branch-point contribution can be obtained using (B-21) the method of steepest descent. In general, oc is *r sinn+(1’2) Bi[A+(&) - k(e,)] obtained by substituting 0=0” in equation (B-11). J B'

In the particular case of two perfect dielectric . eikiR em (fJi-a)&), materials, i andj, forming the boundary, I, where the Hankel function has been replaced by e . -I ki the first term of its asymptotic expansion. The Orij = sin Ki < ki, (B-18) superscripts + and - on A(&) denote the sign of 0 g the radical in equation (B-16) taken in A(&), and and the contour Z?’ runs from t$, to im. The contour B ’ is deformed into the steepest-descent contour, c . -I kj B”, away from 0& The path of steepest descent rYij = sin kj < ki. (B-19) 0 Ki’ is defined by Im ikiR cos (0; - a) = constant (B-22) The steepest-descent evaluation of the branch- point contribution is summarized as follows: The and is illustrated by the dotted line in Figure B-3. branch cut integral has the form On the assumption that kiR>>l, so that only

Downloaded 12/13/19 to 198.120.252.61. Redistribution subject SEG license or copyright; see Terms of Use at http://library.seg.org/ FIG. B-3. Complex B-plane showing modification of saddle-point contour r to contour B in order to account for branch-point contribution, and path of-steepest descent (dotted-line). Radio Interferometry: Part I 579

angles very close to $ contribute significantly tto fB,,d;e-6u(juv‘ f mx2e-si:& the integral, 19ican be set equal to O;iin all expres- 0 sions in the integrand except for the radical. In (B-29) general,

A+(Oi) - A-(ei) = F(Oi) COSBj, (B-23) Rearranging equations (B-24) and (B-28), one and the integral is approximately finally obtains n+l --iki -in(*/2)F(e:j) I* = ___ e--i(2n+l)r/4 ik: e . 2w Ie=_._L-- 2wp2 (k”, - k;yy3,2 (B_3o) l/2 * (1 - cot a tan Oij) sin nf(1’2) O:jF(O”,j) (B-24) . eikip ain 8$jfiki COB @fjZ

cos ejeikiR cm (ei-m)dei. which must be added to equations (B-14) and

B’ (B-15) when cz>cr’. -S The assumption in the saddle-point and steep- For low-loss media, Oil is close to the real axis for est-descent techniques that kR>>l is reasonably kj2s and kR>lO when R>2. integral in equation (B-24) is slightly different in The poles of the integrands are also of im- the two situations, but the results are identical. portance in the solutions. Discussion of their role Here, the Olj will be assumed close to the real axis. in the solutions is given in the text. The approximate solution is valid for Oij near the ?r/2 line. ACKNOWLEDGMENTS Along the steepest-descent contour near &, The author is grateful to the National Research Council of Canada for a fellowship which sup-

tli = et + iu, (B-25) ported this work. This work is the first paper in a series providing where u is much less than unity. Then, the background for the Surface Electrical Proper- ties Experiment planned for the Apollo 17 lunar mission. cos t9j v‘ - Ci*14&i (~-26) REFERENCES Brekhovskikh, L. M., 1960, Waves in layered media: and New York, Academic Press. Budden, K. G., 1961, The wave-guide mode theory of wave propagation: Englewood Cliffs, Prentice-Hall, ikiR cos (Bi-a)zikiR cos (e:j-a) Inc. (B-27) Clemmow,. P. C., 1966, The plane wave spectrum rep- -kiR sin (a-t9t)zJ. resentation of electromagnetic fields: New York, Pergamon Press. El-Said, M. A. H., 1956, Geophysical prospection of The integral in equation (B-24) becomes underground water in the desert by means of electro- magnetic interference fringes: Proc. I.R.E., v. 44, p. 24-30 and 940. - Evans, S., 1963, Radio techniques for the measurement _ &-i*l4,/2 (d-a) of ice thickness: The Polar Record, v. l!, p. 4Oti!O and 795. (B-28) Katsube, T. J., and Collett, L. S., 1971, Electrical prop- perties of Apollo 11 and 12 lunar samples, in Proceed- ings of the Second Lunar Science Conference, Hous- ton, Texas, edited by A. A. Levinson: Cambridge, Mass. Inst. Tech. (in press). Norton, K. A., 1937, The propagation of radio waves

Downloaded 12/13/19 to 198.120.252.61. Redistribution subject SEG license or copyright; see Terms of Use at http://library.seg.org/ Now, the integral over the surface of the earth and in the upper atmo- 580 Annan

sphere, Part I: Proc. I.R.E., v. 24, 1367-1387; in der Drahtlosen telegraphie: Ann. Physik, v. 28, p, Part II: Proc. I.R.E., v. 25, p. 1203-12 9’ 6. 66.5-737. Ott, H., 1941, Reflexion und Brechung .von Kugel- --- 1949, Partial differential equations in physics: we.l$;66Effekle Q. Ordnung: Ann. Physrk, v. 41, p. New York, Academic Press. Strangway, D. W., 1969, Moon: Electrical properties of -- 1943, Die Sattelpunktsmethode in der Umge- the uonermost lavers: Science. v. 165. D. 1012-1013. burg eines Pols mit Anwendungen auf die Wellenoptik Van de; Waerden B. L., 19.51, On the mkihod of saddle und Akustic: Ann. Physik, v. 43, p. 393. points: Appl. Sh. Res., B2, p. 33-45. Rossiter, J. R., LaTorraca, G. A., Annan, A. P. Strang- Wait, J. R., 195.1, The magnetic dipole over the hori- way, D. W., and Simmons, G., 1973, Radio inter- ;;!3% stratrfied earth: Can. J. Phys., v. 29, p. ferometry depth sounding: part II-experimental results: Geophysics, this issue. Wail, J. R., 197$l,.Electromagnetic waves in stratified Saint-Amant, M., and Strangway, David W., 1970, media, 2nd edition: New York, The Macmillan Co. Dielectric properties of dry, geologic materials: Ward, S. H., and Dey, A., 1971, Lunar surface electro- Geophysics, v. 35, p. 624-645. magnetic sounding: A theoretical analysis, I.E.E.E. Sommerfeld, A., 1909, Uber die Ausbreitung der Wellen Trans. GE-g, no. 1, p. 63-71. Downloaded 12/13/19 to 198.120.252.61. Redistribution subject SEG license or copyright; see Terms of Use at http://library.seg.org/