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JOURNAL OF RESEARCH of the National Bureau of Standards-D. Radio Propagation Vol. 64D, No.4 , July- August 1960 Characteristics of 488 Megacycles Per Second Radio Signals Reflected From the Moon 1 B. C. Blevis and J. H. Chapman (Janu ary 18, 1960) Radio signals at 488 m egacycles pe l' sec ond, received after re fl ection from the moon have b een st udied using a cont inuous wave bi stat ic ra dar svstem. located n car Ottawa Ca;l ada. These experimen ts were carr ied out durin g 1957 a nd consisted of mo ni toring the ]' e- c81 ved on two orthogonal dipoles mount ed at the fo cus of a 28 foo t pa ra bolic t r ac kin g a nt enn a. The total mean received signal yielded an e ff ect ive rada r cross s ect ion of t he moon at this frequency of 0.05 of t he projected area. The lib rat ion fading as observed in the two o1'thoo'- onal receiver channels was in synchr onism, with a cross-correl at ion co e ffi cient of 0. 89. It was es tabl isbed that the signal is not on re fl ect ion at the su rf ac e of the moon or in pass in g th rough the ionosphere. Rot at ion of the plane of po lari zatio n of the rad io wave in the double pass age through the ionosph ere was obs r v d to cha nO' e by nearly 180 degrees ov er a six-hour p riod during qu iet ionosph eric condi Lions. . 1. Introduction Signals reflected from the moon have been used for st udying propagation conditions along the path between t lt e earth and Lhe moon and for studyin g the radio refl ection chara cte ri st ics of the moon itself [1 , 2, 4]. 2 Th e st udy report ed in this pap er was begun primarily to inv es ti gate the rotation of the plane of polariz ation a nd Lhe attenuatio n of UHF signal s traversing the ionosph ere. For t hi s reason, plan e polarized waves were tra nsmitt ed from a tracking anlen na, and the signals which were received aft er r efl ection from the moon were monitor ed by two independent receiving systems fed from id entical ortho gonal dipole moun ted in a second tracking antenna. By this means, the ro tat ion of the plane of polariz at ion co uld be observcd and measured ovel' a period of time. Th c measurements were begun early in 19 57 and were continued t hroughout th e ye ar , with var ious changes in equipment and pro ce dure. Both long- pul se [2] and continuous· wave transmiss ions were used. For th e l atter measurement s, it was necess ary to separat e the transmitter and receivers to pr event the very strong transmitted signal from saturating the re ce ivers. For the cw measurements described in this paper , the separation was approximately 60 mile s. Provided the direct signal was sufficiently low, the moon-reflected signal co uld be di st inguished by means of its Doppl er shift. 2. Experimental Method The equipment used during these experiment IS described briefl y in the following paragraphs. The transm itt er was operat ed at a frequency of 488 Mc , with a cw powel' out put of 10 kw . Th e 1 Contr ibution f ro m Defence Research T elecommunicat ion s Establishment Shirley Bay, Ottawa, Canada. ' , Figures in brackets indicate the li tcrature references at the cnd of this paper. t ran smitting and receiving ant ennas used 2 -It parabolic refl ectors with equ atorial mount s and dri ve sy.stems. cO l'rection on each axis pcr- mltt ed. ulllnt cl'rupt ed trackmg of the moon from moonn e to moonset. Th e transmitted ra diation was essentially plan e- polarized. Two id entical re ce iving systems with noise fi o' ures of about 7 db wore fed from orthogonal cli p ole anLennas mounted at th e fo cus of the receiving parabolic re f! ectol'. Th e tran smiLler frequen cy and Ll lC fU'st two local oscillatol' inj ection frcquenci es of the receivel' were co ntrolled from similar cry Lal sta ndard s with an overall stability of Lhe ordcr of 1 part in 10 8 . Th e receivcr output at the second IF was th en mi xed with th e signal from a stable VFO to give a third IF at a ce nt cr frequency of 425 cp s. Th e varying Doppl er slnIt [ 2] due Lo the relative motion of the moon and the point of ob e rva tion was eliminated by continual adjustment of thc VFO to maintain a stablc Li ssajous pat tern on an oscilloscope. In this way , the 425-cps output could be passcd Lhl'ollO'h a fixed narrow band (90 filter. Th e signal b was then recorded on magn e tlC tape for subse qu en t analysis, also detect ed and d isplayed on paper chart recordmgs. 3. Signal Characteristics 3.1 . Farada y Rotation . Th e rotation of the plane of polariza- tlOn of a radlO wave pass ing through the ionosphere has been dcscribed in d etail in thc lit eratme [1]. A ':,hi ch. exhibit s the etl' ects of Faraday 1'0- tatlOn IS glven Jl1 figure 1. This record was made d a of ionospheric con- dltl.ons. Ih e rota .tIOn of the plane of polari- zatlOn of t he Signal durmg fi. 6-hr period is evident from a comparison of the two traces which come 33 1

Characteristics of 488 megacycles per second radio signals ...Characteristics of 488 Megacycles Per Second Radio Signals Reflected From the Moon 1 B. C. Blevis and J. H. Chapman

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Page 1: Characteristics of 488 megacycles per second radio signals ...Characteristics of 488 Megacycles Per Second Radio Signals Reflected From the Moon 1 B. C. Blevis and J. H. Chapman

JOURNAL OF RESEARCH of the National Bureau of Standards-D. Radio Propagation

Vol. 64D, No.4, July- August 1960

Characteristics of 488 Megacycles Per Second Radio Signals Reflected From the Moon 1

B. C. Blevis and J. H. Chapman

(January 18, 1960)

R adio signals at 488 megacycles pel' second, received after refl ec tion from t he moon have been studied usin g a continuous wave bistatic radar svstem. located ncar Ottawa Ca;lada . These experiments were carried out durin g 1957 a nd consist ed of moni torin g t he ~ i gna l s ]'e­c81ved on t wo orthogonal dipoles mounted at the fo cus of a 28 foo t pa ra bolic t rackin g a ntenn a. The total mea n received signal yielded an effective radar cross section of t he moon at this frequency of 0.05 of t he projected a rea. The lib ration fadin g as obse rved in the two o1'thoo'­onal receiver cha nnels was in synchronism, wit h a cross-correlation coeffi cient of 0. 89. I t was establ isbed t hat the signal is not depo l f'lri~ed s i ~ nificantly on refl ection at t he su rface of t he moon or in pass in g th rough th e io nosphere. Rot ation of the p lane of polari zation of the rad io wave in th e doubl e p assage t hrough the ionosphere was obs r v d to cha nO'e by nearly 180 degrees over a s ix-hour p riod during qu iet ionospheric condi Lions. .

1. Introduction

Signals reflected from the moon have been used for studying propagation conditions along the path between t lte earth and Lhe moon and for studying the radio r efl ection characteristics of the moon itself [1 , 2, 4].2 The study reported in this paper was begun primarily to inves tigate the rotation of the plane of polariza tion and Lhe attenuatio n of UHF signals traversing the ionosphere. For this reason , plane polarized waves were transmitted from a tracking anlenna, and the signals which were received after r eflection from the moon were monitored by t wo independent receiving systems fed from identi cal orthogonal dipole mounted in a second tracking antenna. By this means, the ro tation of the plane of polarization co uld be observcd and measured ovel' a period of time.

Thc measurements were begun early in 1957 and were continued throughout the year, with various changes in equipment and procedure. Both long­pulse [2] and continuous· wave transmissions were used. For the latter measurements, it was necessary to separate the transmitter and receivers to prevent the very strong transmitted signal from saturating the receivers. For the cw measurements described in this paper, the separation was approximately 60 miles. Provided the direct signal was sufficiently low, the moon-reflected signal could be distinguished by means of its Doppler shift.

2 . Experimental Method

The equipment used during these experiment IS

described briefly in the following paragraphs. The transmitter was operated at a frequency of

488 Mc, with a cw powel' output of 10 kw. The

1 Contribu tion from Defence Research Telecommunications Establishment Shirley Bay, Ottawa, Canada. '

, Figures in brackets indicate the li tcrature references at the cnd of this paper.

transmit ting and receiving antennas used 2 -It parabolic reflectors with equatorial mounts and drive sy.stems. ~mall cO l'rection ~lotors on each axis pcr­mltted. ulllntcl'rupted trackmg of the moon from moonn e to moonset. The transmitted radiation was essentially plane-polarized.

Two identical rece iving systems with noise fio'ures of about 7 db wore fed from orthogonal clip ole anLennas mounted at the fo cus of the r eceiving parabolic ref! ectol'.

The transmiLler frequency and LllC fU'st two local oscillatol' inj ection frcquencies of the receivel' were controlled from similar cry Lal standards with an overall stability of Lhe ordcr of 1 part in 108. The receivcr output at the second IF was then mixed with the signal from a stable VFO to give a third IF at a centcr frequency of 425 cps. The varying Doppler slnIt [2] due Lo the relative motion of the moon and the point of ob ervation was eliminated by continual adjustment of thc VFO to maintain a stablc Lissajous pat tern on an oscilloscope. In this way, the 425-cps output could be passcd Lhl'ollO'h a fixed narrow band (90 cps~ filter. The signal bwas then recorded on magnetlC tape for subsequen t analysis, an~ also detected and d isplayed on paper chart recordmgs.

3. Signal Characteristics

3.1 . Faraday Rotation

. The Fal'a~fi.Y rotation of the plane of polariza­tlOn of a radlO wave passing through the ionosphere has been dcscribed in detail in t hc literatme [1]. A rec~)l'dil?g ':,hich. exhibits the etl'ects of Faraday 1'0-

tatlOn IS glven Jl1 figure 1. This record was made d ~l~'in g a ~~rjod of rclati\~ely q~jct ionospheric con­dltl.ons. Ihe ~low rota.tIOn of the plane of polari­zatlOn of t he Signal durmg fi. 6-hr period is evident from a comparison of the two traces which come

331

Page 2: Characteristics of 488 megacycles per second radio signals ...Characteristics of 488 Megacycles Per Second Radio Signals Reflected From the Moon 1 B. C. Blevis and J. H. Chapman

F IGURE 1. Fam day Totation Tecord.

Comparison of the relati\'e signal on two orthogonal polarizations o\'m a 6-hr period on 15 September 1957.

from the two orthogonal receiver channels. Thc broadening of the record is due to the libra tion fading, as discussed below, which is partially smoothed by pos t-detection in tegrat ion . Timing marks on the record were made by shut ting t he transmitter off every 15 min. Receiver noise call be seen during these periods .

Upper t ransit of the moon occurred just before the beginning of this record, and the moon was t racked down to the horizoll. The increase of signal near the end is a t,tributed to constructive inter­ference betwee n t he direct and ground-reflect ed signals just beforc moonset.

This record was obtained during the morning when the t otal electron content of the ionosphcre was increasing towards its m aximum. In addition, the amount of rotation due to the increasing path length t hrough the ionosphere was also increasing. It is reasonable t o assume, therefore, that the ro­tation of t he plane of polarizat ion was monotonic, and hence a t otal change in rotation of almost 180 deg is indicat ed .

The difference in signal levels between the two orthogonal channels during periods when the r e­ceived signal was nearly all in one of the t wo chan­nels, or between maximullls and minimums on a single channel, has been observed to be as great as 16 db . The isolation between the feed dipoles was 40 db wh en measured alone, and although this value was somewhat reduced wh en the dipoles were mounted in front of t he reflector, t he isolation was still greater than the measured differences between channels.

3 .2 . Libration Fading

Fading due to libration of the moo n is generally deep and rapid, being as fast as several cycles per second during periods of maximum libration rate. This fading is due, of course, t o the ch ange in rela­t ive path lengths of signaJs scat tered fro m dif­feren t portions of the moon 's surface.

A typical expanded recording covering a 35-sec period is showll in figure 2. The signal was about

2 rl ------~--------._------,-------,_------_,------_.--------_,

w o ::0 0 t: a. ~ 4

o 10 20

TIME, sec

F IGURE 2. Libmtion fading.

30

A 35-sec recording of the amplitude of signals on two orthogonal polarizations. 'rhe recording time constant was 0.4 sec.

332

Page 3: Characteristics of 488 megacycles per second radio signals ...Characteristics of 488 Megacycles Per Second Radio Signals Reflected From the Moon 1 B. C. Blevis and J. H. Chapman

~wice as strong in the upper chann el but an ad­justment of the recorder gain has compensated for ithis. The depth of fading will be limited by the 3ffectivc bandwidth or amount of post-detect ion integration. However , in this example, with a time constant of 0.4 sec, the signal still fades into . . DOlse on occaSIon.

The signals are seen to be well correlated in the two receiving channels. Several analyses of this correlation have been perform ed. A typical example is illustrated by figure 3 which shows a scaLter plot of the signal amplitude on the two channels at 0.8-~ec intervals during a I-min period. Machine cal­~ulations indicate a cross-correlation coeffi cient of 0.89.

w o ::J >­:::i Q.

;:, <t

>-

6 r-----------,------------.-----------,

/ M .. ,y .. ::::. .Ie . .. ,

:::. e.- • / ' ,

OL-__________ ~ __________ ~----------~

o X AMPLITUDE

FlGURE 3. Scatler plot 0/ the relative signal amplitude on orthogonal polari zations.

An amplitude of zero corresponds to the noise level.

l The amplitude distribution of the signal on jther channel approximates that of a Rayleigh :listribution as can be seen by figure 4, which is a logarithmic plot of the probability density in alH­olitude. The amplitude is given in arbitrary units . these data were obtained by sampling the amplitude ~f a 5-min section of record at a sampling frequency of 1 kc.

From the analyses in this and the above section, pne cn,n con elude that there is lit tle depolarization of I;h e signal on reflection at the moon's surface or in ~ts passn,ge through the ionosphere. The plane ;lOlarized signal, which was transmitted to the moon, :s received on the earth with the plane polarization iargely preserved.

3.0

2.5

2.0

I .5 L-______ -'-______ ---l'--______ ....I-______ ---'

o 400 800 1200 1600 R2

F l GURE 4. Log plot of the probability density function. R is the signal amplitude on a si ngle channel ill arbitrary units, p(R) its proba·

bi li ty density.

3.3. Total Signal Power

A number of calculations h ave been made of the total signn,l power receivcd by adding vectorially the signals in each channel. Assuming antenna ga in of 30 db, the corresponding effective cross section of th e moon is calculated to be of the order of 5 X 10 11m 2 or 0.057ra2, where a is the lunar radius. The ultcer taint, · in this result is believed to be less than 3 db. "

When these experiments began in F ebruary 1957, there were t imes when the total signal was un ac­co untably low for periods of t he order of an hour or so. The apparent loss of signal was about 6 db or more. The times when this phenom enon oc­curred did not appear to correlate with tho position of the moon above the horizon [3]. Investigations at the time were thought to rule out the possi­bility of any equ ipment malfunction .

Subsequently fairly exhaustive s tudies have been made in an attempt to repeat these observations under carefully controlled conditions using superior equipment [4]. The results have been negative, in that the total power was obser ved to remain ensibly constant within a decibel or so. It is coneluded that either the physical conditions responsible for the earlier loss of signal were not duplica ted during the subsequent tests , or that some still unknown equip­ment factor was responsible.

4. Conclusions

The F araday rotation of the rad io signal tr aversing the ionosphere in two directions ha been observed to change by nearly 180 deg over a 6-hr period during quiet ionospheric conditions.

From an analysis of the rapid fading of the signal due to libration of the moon and of the difference in signal power between cross-polarized components,

54432S- 60-3 333

Page 4: Characteristics of 488 megacycles per second radio signals ...Characteristics of 488 Megacycles Per Second Radio Signals Reflected From the Moon 1 B. C. Blevis and J. H. Chapman

it is concluded that the transmitted polarization is largely preserved on reflection from the moon's surface and that the surface is probably not deeply serrated and rough, at least at this wavelength (62 cm).

The effective value of the lunar radar cross section at 488 Me, obtained by adding vectorially the mean signal on orthogonal polarizations, is of the order of O.057ra2 as measured with a cw radar.

The results of more recent experiments carried out jointly by Lincoln Laboratory of M.LT., the Stanford Research Institute, and the Defence Re­search Telecommunications Establishment have been published elsewhere [4).

The authors acknowledge the assistance of their colleagues, particularly F. D. Green, H. V. Serson, and E. A. Oameron, in making these measurements.

334

5 . References [1] 1. C. Browne, J. V. Evans, J. K . Hargreaves, and W. A. S

Murray, R adio echoes from the moon, Proc. Phys Soc . B 69, 901 (1956). I

[2] B. C. Blevis, Ionospheric studies by t he lunar radal technique, Nature 180, 138 (1957).

[3] S. Rush and L. Colin, The effects on radio astronomica observations due to longitudinal propagation in til( presence of field-aligned ionization, Proc. I.R.E. 46 356 (1958). I

[4] J. C. James, L. E. Bird, R. P . Ingalls, M. L. Stone J . W. B . Day, G. E. K. Lockwood , and R. 1. Presnell Observed characteristics of an ultra high freqnencj signal traversing an auroral disturbance, Nature 185< 510 (1960) .

(P a per 64D4- 65:

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