SCIENTIFIC ABSTRACT SOROCHENKO, A.A. - SOROCHINSKIY, V.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001652430001-9
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: August 26, 2000
• Sequence Number: 1
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

YV,VDOXIIIUVA, it.l.; SOMMMKO, A-Al.
Plastics based on othvlcellulose and butyrate acetate cellulose.
Biul.tekh.-ekon.inform. no.1:10-12 159- (MIRA 12:2)
(Plastics) (Cellulore)

MOD
87652
5/191/60/000/003/001/013
Bo16/BO54
AUTHORS: Pechenkin, A. L., Yevdokimovaq A. I.,
TITLE: Plastics (Etrols) on the Basis of Cellulose Eaters
PERIODICAL: Plasticheskiye massy, 1960, No. 3, pp. 2-8
TEXT: The authors report on their study of compositions and applica-
tions of etrols. 1) Acetobutyrate cellulose etrol (ABCE). Resistance to
water and frost, and compatibility with plasticizers increase with in-
creasing content of butyryl groups in this eater, while its heat resis-
tance decreases. The physicomechanical characteristics as dependent on
the plasticizer used are given. Hence, the authors conclude that, among 4,1
all plasticizers studied, dibutyl sebacinate offers the strongest re-
sistance to frost. Triphenyl phosphate gives a higher hardness and
strength in static bending. Dioctyl phthalate gives better characteris-
tics of resistance to heat and toughness. The following plasticizers
were also tested: dibutyl phthalate, dioctyl sebacinate, tricresyl
phosphate, dibutyl adipinate, and EA-242 (YeD-242). Salol, as well as
mixtures of resorcinol dibenzoate with 1,3,5-tritertiary butyl phenol
Card 1/3

87652
Plastics (Etrols) on the Basis of cellulose S/191/60/000/003/001/013
Esters B016/BO54
(ff-23, P-23), and of salol with P-23, proved to be the most efficient
stabilizers. Besides, the authors studied: p-octyl phenol# p-amyl phenol,
resorcinol disalicylate, and resorcinol dibenzoate. The authors give
the physicomechanical characteristics of four ABCE types developed by
NIIPP (Scientific Research Institute of Plastic Products): A943-45-20
(ABTaE-45-20),and ASP-38-20 (ABTaE-38-20), both for lining steering
wheels and for the production of small workpieces; ASO-38-12
(ABTsE-38-12) and ASq3-45-8 (ABTsE-45-8) for the production of thin-
walled workpieces without reinforcement and larger parts of motor ve-
hicles in temperate and tropical climates. This substance is also suited
for the radio industry, for the production of musical instruments, spec-
tacle frames, incombustible toys, and the like. 2) Acetopropionate-cellu-
lose and tripropionate-cellulose etrols, as compared with ABCE plastics,
have better mechanical properties, resistance to heat and water, can be
easily dyed with various colors, and have a more decorative look. Best
plasticizers for them were: mixtures of dibutyl phthalate and dioetyl
phthalate. The following types were tested: 00-48-30 (APTOB-48-30),
-48-15; -33-30; -33-20; T94)-64-20 (TPTsE-64-20), and -64-15. They are
suited for the production of motor-vehicle parts, door handles, radio
Card 2/3

82774
SOV/184-59-5-1/17
AUTHORS: Soroche Korobchanskiy, O.A., Engineers
TI TLE An Automatic Filtering Centrifuge With Sediment Removal by a Knife
PERIODICAL: Khimicheskoye mashinostroeniye, 1959, Nr- 5. PP. 1-3 (USSR)
ABSTRACT: The first industrial model of the "Ar-1,2OO-2Y " (AG-k2OO-2U) filter-
ing centrifuge with sublayer regeneration by outside washing is
described. The centrifuge was manufactured at the imeni Frunze
plant in Sumy. It was tested on the regeneration of foundry loam
under unfavourable conditionsbecause the pulp had a clay component
and the sand had sharp edges. In the standard periodic action
automatic filtering centrifuges the sediment cannot be removed
entirely by a knife. The authors designed a specii! rotor and a
sublayer regeneration device for centrifuging suspensions with both
soluble and insoluble solid phases. The filtering base is a shell
formed by a helically wound wire of trapezoidal cross-section having
a clearance of 0.2-0.3 mm between wires. This sieve is fixed in the
rotor (Fig. 2). The regeneration of the filtering base and the sub-
layer is performed by a strong water jet directed from outside to
the rotor. The water sprayer moves reciprocally parallel to %he
Card 1/ rotor axis. The servomotor and the water supply are switched ::. -,i V@

82774
sov/0-59-5-1/17
An Automatic Filtering Centrifuge With Sediment Removal by a Knife
relays. Tests were carried out on the "Ar -6oo" (AG-6oo) semi-industri-
al centrifuge, confirmed the possibility of separating the molding
loam suspension under conditions of full automation. Figure 6
shows an operational diagram of the AG-;2OO-2U cMtr1fuge. The
washed sand passes from the classifier into the container M-4th a
mixer (1) placed 1,5 m above the feed pipe of the centrifuge (2).
The pulp Is fed to the centrifuge through an automatic charging
valve (3) In the bottom of the container. The separated liquid and
the washing water are drained through a common pipeline into the
settling tank. The centrifuge worked under the following conditions:
RPM - 4.30; sandlayer thickness - 85 mm; sublayer thickness - 8 mm;
pulp composition; sand - 68%, clay - up to 2%, the reat was waterl
water pressure for regeneration in the.sprayer - 6 kg/cm2j the---
removal of the fine solid phase with the separated liquid - 23..5'9/1.
The different phases of one operating cycle of the centrifuge were;
charging - 20 see, centrifuging - 60 see, discharging - 25 sec,
regeneration of the sublayer - 60 sec, total - 2 win, 45 sec. The
efficiency of the centrifuge was 4,600 kg/hour of sand dried to a
humidity of 3.8 4.8%. Characteristics of the centrifuge are%
Card 2/3 rotor diameter 1,180 mm; rotor speed - 430 rpm, electricmoto-

8277h
sov./i84-59-5-1/1'7
An Automatic Filtering Centrif).ige With Sediment Removal by a Knife
10 kw; rotor volume - 240 1; weight of the centrifuge - 7,600 kg.
During 100 hours of industrial tests the knife and the comb of the
level regulator (easily removable steel parts with a hard alley
surface) had to be exchanged once. Other parts exposed to the pulS@
had no noticeable wear. The relatively low speed of the rotor is
sufficient fcr the purpose described because of the good filtrability
of sand. For centrifuging intermediate products of the plastics
production, e.g. polyvinyl chloride resin suspensions, polyethylene
and others, the rotor spted can be increased to the values necessary
for each particular case and the liquid pressure for regeneraticn
can be increased to 8-10 kg/'cm2. There are 2 photographs, 2 diagrams
and 2 graphs.
Card 31@

Meteorological Abst. 4.8-157
Vol. 4 No. 8 Bulavko, A. C. and Sorochenkov X. Ke Vookhodis#hehie
Aug. 1953 vozdGVn-yapotok1 re -o----s-iTy-.' Vertical air current
Part I of unusual force.) Meteorologiia i Giarol;g-Tra-t-lo.
Pressure and Wind 7-.28-30t 1952. DLG-Two parachutists were dropped
over the Borisov Region (Minsk province) at 5:30 p.m.
of August 1, 1950 and landed, the first after 40 mint
and the second after 2 hrs. The probable lift of the
second one is assumed to be 3 km. The region was
located in an area of diffused pressure fieldo with
secondary cold frcnt passing by and powerful cumulus
clouds. The two layers of cumulus had bases at about
1200 m and 3100 m. Air temperature near the soil
surface was 18-20'C, lapsc rate was 0.7-080. Thunder
activity was reeistered In the region from afternoon
to 8-9 p.-n. Sub#ect Headings: I. Vertical currents
2. Borisov Region. U. .3. S. R. --4. T. Z.

SOROCHEKKOI P.
Two hundred houses for collective farmers. Sill. bud. 7
no.5.-4-6 Kr 157. (NMA 13:6)
1. Predeedatell soveta methkolkhosnoy Btrottellnoy orgRnItat-
sit to.1 Cherkasekogo rayona, Cherkseekoy oblasti.
(Charkasay District--Yarmbouses)

SONC111=01 P.
flow we achieved success in our Vork. Sill.bud. 8 no.2:7-6 F
158, (MIRA 13:7)
1. Predsedatell soveta Cherkassko7 mezhl-olkhoznoy stroitellnoy
organizateii No.1 Cherknoskoy obInstlo
(Cherkassy Province-Builiing)

zn
F,
UWRAkstronomy - Radio AstronomW Nov/Dee 53
"Interference Radio Telescope," V.V. Vitkevich and
R.L. Sorochenko, Phys Just im Lebedlev, Acad Sci USSR
Astron Zhur, Vol 30, No 6, pp 631-635
Discusses an antenna system consisting of a series
of separate antennas of small dimensions and
coupled electrically. He compares this diagram of
radio reception to optic Interference pattern by
a diffraction grid. Considers this system. as more
advantageous than others. Rec 20 Apr 53.
2T3T75

C,ttegory USSR/Radiophyaice - Application of radiophysical methods 1-12
Abs Jour Ref Zhur - Fizika, No 1, 1957 No 200B
Author Chikhachav, B.M., Sorochanko R.L.
:Apparatus for the - -_ _jhe 21-ca Hydrogen Radio-Wave Spectral Line
Title
Orig Pub :Tr. 5-90 soveshchaniya PO vopr. kosmogonii. 1955, @-, AN SM, 1956, 546-549,
diskus. 550-553
Abstract :The apparatus is based on the principle of the frequency radiometer with
double frequency convarsion. A balanced method Is nied, in Vhicb tvo nor-
row-bond filtere.soparated in frequency and two second heterodynes alter-
nately switched at a modulation frequency of 360 c*lesp are connected to the
output of the second i-f stage. Ma this caseoscillstions'froa one oftva
fixed portlons of the spectran under investigations Are alternately passed
through each filter. The Ofference in the intensity6f the noise at the
outppt of the filters is?,vopbzrated by a balanced detector. Tho &-c campoment
at the modulation frequency appears at the output of the belanced dotwtor
only in that case, vhen the spectral densities of the noise in the fftiid por-
tions differ from each other. The search for the line is effectt4 by varying
the frequency of the first, heterodyne. The frequendies of the first and
second heterodyn6a and the n&rrrv-biuA filters are crystal-stabilized. fte,
accuracy of the meaeurement of the line frequency in 1.5 kc. The sensitivity

t@ 11' 2 86
31W 14 /60/OW/ CX@t/fX5 lVj,'
0 AjoF,/Ao26
AUTHOR: S(,--rochenko, R.
T ITLL,, conve I*SdL loll Ovmr 1a) Light Years
PERIODICAL. Znaniye-Sila, Ic,)60, No. 8, pp. 6-7
TEXT: A new field of science - raciloastronomy - started Its stozmy develop-
ment. Standing in t,17e middle between radlo--physics and astronomy it may, te3ldes
astronomic problems, solve the riddle whether there is life in other parts of the
Universe. The first step toward this aim is to get signals from the Universe;
an artificiall signal, not a natural one. Radloelectromagnetic tests lately proved
that space surrounding the earth intensively emits waves, the inter-sity increas-
ing with the length of the wave. The most favorable wave for cosmic radlocommu-
nications seeM3 to be the length between 3 and 30 cm. Within this range thore
Is the 21 cm wave being of major importance In radioastronomy, because this wave
Is used for, transmission by interstellar hydrogen. Every atom of hydrogen Is
a midget radiotransmitter, emitting a "portion" of electromagnetic energy of
fixed magnitude, the frequency be!ng conditioned by the inner structure. The
Intensity of this transmission is not too high and may easily be covered by an
artificial signal. Hydrogen is tb-@- mo3t abundant element in the Universe. Not
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86286
S/004/60/000/006/005/005
Conversation Over 100 Light Yeare A105/AO26
long ago, American scientists logica.!;y- pr,!.qupposed that Ir there should ext.,st,
a civilized community somtwhere on other plwimtary systems Investigating
space, it would draw the same conclusions and consequently choose a 21 cm wave
for communication; furthermore, If such civilized community Is In possession
of a system of guided transmission Into all direotions, It coull get a contact
with our solar eyatem. As for the range, the level of our electrote@lhnical know-
ledge permits realizing contact over a distance of 100 light years. Some months
ago, an outstanding radlotachnioal experiment has be,!n ac!@omplished by radiolo-
eating the planet Venus. In this experiment a transmitter sending 265 kw waves
was used. An immense anter-na was concentrating waves Into a beam directing t1".em
to Venus. Thus, the effielency of transmis.Aon was amplified more than seven
thoueand tlmes,i.t., two million kw. Sptuolai receivers for weRk signals achlevad
an enormous sensitivit@. Thty WOT'k. Wltb huge antennas collecting signals on an
area of thousantbof km Amplification of Tte- rtcnived sigpial is done. by spe,Dial
molecular and parametric devices. Inzide the sphere with a radius of 100 light
years there are about ten thnusand start@. Only few of them have planetary sys-
tems, and consequently. a basis for the exI.!Oenct of life. There is eoms.4 pr-,r,3,.
bility that at least one of these stars has a olvilized comrinitj with a Mg)-ay
developed culture and technical '@n the USA, a tpecial apparatus is
under constru@*'Ion at, pr,!-sent. for trar,.Wliqion of oilgrt&la cra 21 @,m OK,
Card 2,13

8L
S/02bj6o/132/01/21/064
B01 4/BOI 4
AUTHORS: Vitkovich, V.V., Sorochenko, R.L., Udal tsov, V.A.
TITLE: Radioaetronomical Oboe-.a'.1r-8 of the Second Soyiet CosajL_lg"
PERIODICAL: Doklady Akademii nauk SSSR, 19tO, Vol. 132) So# It Pp. 85-88
TEXT: The frequently used method of -.-aalointerference was employed for oNeerving
radio signals of the second Soviet oo.mic rocket. The angular coordinates of the
container were measured by means o: -%e wientific instrwients, furthermore the
power of the signals received and its vEriationa with time, A buzzer signal
was i-A because of the increased stability of the instruments, the first and
aeo -eterodyne were stabilized by means of quartz. The distance 'Ket'.Teen the
antE @s of the radiointerferometer, which were directed to the east, was
175-P m. The angle between the perpendicular on the line o3nneoting the
antennas and the direction to the signal source was measu ,-;'A by means of the
radiointerferometer. Formula (1) is given for the determina-cion of this anglep
and formula (3), in which the Doppler effect is considered, is derived for the
azimuth of the signal source. The radiointer0ercAeter is adjusted according to
Card 1/3 \11 V

811K60
aadicastronomical Observations of the Seooild S/020/60/132/01/21/064
50-Tiet C03Mic Rooke. BO14/BO14
the irtsmait- of ac-smio radio sources. This a., - ;um permitted exaot determination
0j. the momdui at which tLq Soviet rocket hit the Moonp as well as of the place
at which the container is located. Fig. I shows a copy of the rooorded signal in
the final stage of the rocket's flight to the Moon. It Is shown that the
reoording loot its sinueoidal --iharacter (oaused by interferences) as soon as the
eontairter hit t@- Moon., The rooket reaohed the Moon on September 14s 1959,
0 h 2 min 22 aso, The place of the oo..tainer was established from formula (3)
and is shown In fig, 3, The power of the signs' received was determ:Lned by
oompVIng it with the Intensity of the cosmic radio souroo of Cygnus-A. Fig. 3
Parther Illustrates rp@ordivgs made during the last days before tho arrival of
the rooket on the Moon. Periodiz intensity variations of 45 soc-onds, 45 minutes,
and 10 -- 13 minutes aere observfd. In this connection t%e authors r0ifer to the
periodic variation in the orientation of the container and to the Faraday
effect detected in the ionosphere. There are 3 figures, I table, and 8 references,
7 of which are Soviet,
ASSOCIATION; Pizioheskly institut im. ?,I. Lebedeva Akademii nauk SSSR
@hysics Institute Imeni P.R. Lebedov of the Academy of Sciences of
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2W8
s/36o/61/000/007/002/010
3, 0 0 (/ 0 E032/E114
AUTHORSs Vitkovich, V.V., Kuzlmin, A.D., Sorochenko, R.L.9
and Udalltsov, V.A.
'rITLE; Results of radio-Astronomical observations obtained
with Soviet space rockets
PERIODICAL: Akademiya nauk SSSR. Iskusstvennyye sputniki Zemli.
No.7. Moscow, 1961, pp. 23-31
TEXTt An important problem in satellite and rocket
experiments is the determination of the coordinatps of the space
vehicles. Since the satellites and rochttm usually carry a
4tabilized transmitter, the problem is reducr-d to the determination
of the position of the radio source and is analogous to the radio-
astronomical problem of the determination of the angular
coordinates of discrete sources. Such determinations are usually
carried out by the radio-interferometf@r method. The present
authors have used this method in the observation of the radio
signals from the first, second and tbird Soviet spal-e rockets.
The use of radio astronomical methods ba.4 enabled them to measure
the intensity of the signals as well. The (0j.,;ervations were
carried out on 183.6 Mc/s. The apparatus jr1l thp e?xpertmental
Card 1/8

26653
Results of radio-astronomical .... s/56o/61/(100/007/002/010
E032/E114
method employed are described by the present authors in Ref.1
(Radlotekhnika i elektronika, 1961). The impact of the second
space rocket container on the lunar surface oi-curred on September
14, 1959, at 0 hr 02 min 22il sec (this time is corrected for the
time of propagation of the signal). rho selenographic coordinates
of the centre of the region of impact were found to be:
latitude 300, longitude -30 (crater Archimedes). During the
observations of the first and second space rockets use was made of
antennas with horizontal polarization. It i3 clear from the
records obtained that in addition to a "quasi-sinusoidal" intensity
variation due to interference there were also faster changes,which
were apparently due to the rotation of the container. The period
of these changes was 30-50 sec for the first and 40-60 sec for the
second rocket. Comparisons of the records of signals from Soviet
space rockets with those for known discrete sources of radio
emission were used to estimate the intensity of the signal
throughout the entire period of observations. The Cyg A source
was used for the comparison. Figs. 4 and 5 show the variations in
the intensity of the signals (slow component) in units of the
power reduced to an isotropic emitter at the distance of the
Card 2/8

26658
Results of radio-astronomical s/56o/61/000/007/002/010
E032/E114
rocket. A consideration of these curves shows that in addition to
the fast changes mentioned above there were also slower variations
in the signal ftm the first space rocket (characteristic periods
8-12 min and 40-60 min). In the case of the second rocket there
was a period of 45 mim reducing to 10-13 min. These changes may
be due to the rotation of the container and the Faraday effect in
the earth's atmosphere. In the case of the third rocket antennas
with both horizontal and vertical polarization were employed.
Typical records are reproduced. Analysis of the intensity records
with two mutually perpendicular polarizatiors showed that there was
signal fading on October 11, 5, 6, 12 and 1.7, 1959, with a period
of about 3 min. In addition there was a signal variation reducing
the amplitude to about 509o' which had a pertod of about 1.5 min.
These variations are apparently diie to the rotation of the
automatic inter-planetary station. There was some evidence that
there was a further variation with a period of 20-30 min, and this
may be due to the Faraday effect. The energy flux p was
calculated from the expression
P = J&f m
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26658
Results of radio-astronomical s/56o/61/000/007/002/010
E032/EI14
where j Is the energy flux from a litecrete source with a
cont inuous spectrum, 6 f Is the bandwidth of the rece-I'ver used to
record the discrete source, and m ts the ra t it) or the space
rocket to discrete-source signal. V@- emitted power P was
calculated from: P - P47R2
where R Is the distance from the earth (isotropic source emitting
equally in both polarization components".
There @re 7 figures and 7 references: 2 Soviet and 5 English.
The four most recent English languags references reads
ReC.4: P. Moore, Nature, V.184, 502, 19@9.
Ref-5: H.P. Wilkins, Nature, V.184, 502, 1959@
Ref.61 G. Fielder, Nature, V.185, 11, 196o.
Ref-7s G. Whitfield, Paris Symposium on Radio Astronomy, Stanford,
California, 1959, p. 299.
Card 4/8

W"
2851
@61/006/009/001/018
D201/D302
4.41. 3 x 0
AUTHORS: Vitkevich, V.V.0 Kuzlmin# A.D.9 Matveye%ko, L*I#o
Sorochenko, R.L., and Udalltsovp V.A.
TITLE: Radioastronomical observations of Soviet- cosmic
rockets
PERIODICAL: Radiotekhnika i elektronika, v. 6f no# 90 1961t
1420 - 1431
TEXTs This is a description of a apecially designed radio inter-
ferometer with phase modulationj as used in tracking the first
three Soviet space rockets. The principle of a two channel phase
divergent reception was used to detect changes in the signal ampli-
tude, due to relative changes of the position of transmitter with
respect to the lobe of interference diagram. In receiving a signal
with continuous spectrum the fluctuation sensitivity in units of
temperature (Ta) of the antenna is given by the well known equa-
tion
Card 1/7 ox

2@)518
S/109/61/'006/009/001/018
Radioastronomical observations D2_011D302
ST a n '1'o'e V_@EfT (7)
where ct a dimensionless factor depending on the properties of
the receiver, T 0 - standard ambient temperature; Pe = + T in)/
/T - the equivalent input temperature determined by noiLe of the
0 1 %;,
receiver; Tin = (F - 1); F - noise factor of the receiver; T -
r Ir!, a
antenna temperature; T - time constant of the output cct;I@f -
passband between input and detector. The bloc diagram of the recei-
ver is shown; the operating frequency was 183 .6 Me/a, that of the
transmitter in the rocket capsule. The interferometer had two pa-
rabolic antennae 8 x 16 and 11 x 28 m, spaced in the E-W direction
by approximately 176 zi. Total length of both antennae was 8 m. The
antennae were reilluminated from their focal points by specially
designed radiating systems, assuring best possible illumination for
two linear polarizations perpendicular with respect to each other.
Yu.P. Ilyasov participated in their design. A schematic of the LAY
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S/109/61/006/009/001/018
Hadioastronomical observations D201/D302
illuminating system is also shown, the three resonant dipoles were
connected by equal lengths of a PK-20 kRK-20) cable to a common
feeder. The directional patterns and utilization factors of the an-
tenna areas were determined from solar radiation. For both antennae,
the area utilization factor was about 0.5. Phase modulation at a
frequency 72 c/s was alieved by changing the phase by 1800 by mean!5
of periodical variation of the electric length of the wall connect-
ing the local oscillator with one of the mixers, so ihaL ths re-
ceived signal was amplitude modulated at this frequency. The phase
modulator was designed around a standard hybria switCh. The switch-
ing elements were light house diodes type 6A 39 (6D3D) driven by
the sinusoidal modulating voltage. The attenuation introduced did
not exceed 2 db. The change in the diode slopes by way of changing
.he bias and the inser-tion of the modulator into the local oscilla-
tor circuit permitted the parasitic amplitude modulation of earlier
systems to be reduced considerably. The modu:ator used permitted
the radio meter with pnase moaul'ation to be changed into that with
AM, this was achieved oy suppressing the modulating voltage at one
of the diodes. The s-@gnaIs were preariplifted a-.. UHF by amp.Lifiers
Card 3/7

S/1,39/6 !/ 006/009/00 1 /018
Radioastronomical observations D20./D302
placed directly at 'the antennae. The noise factor of UNP preampli-
fiers was 5. The amplitied signals from each antenna were changed
after buffer stages ro :IiE let IF of 6.95 M_-/s and fed into two
channels with a 90',; phase shift between them. A double frequency
conversion was ueed. Tbs! 19C% 554 mc/s frequenry of the first 1c-
cal oscillator wac pr:a,.-c-@tj by a thermostatically controlled cry-
stal oscillator workinp a@t 9,074 mc/a with subsequent multiplicu-
tion by 21. Its re_@a-,!ve njtabJL.'.ity was '&_6 and hence the pass-
band of a monochrom,,t-c aignal was chosen to be M/s. To secure
reception with. ths. s-_gna ., frequency ahlf-cing due to the Doppler
effoct, step tu.-ling vv_@ "nI-. k".1 Kc/s was p.-ovided formed by 5 1-ezc-
nant circuits datuncl, in @ irl,/s steps. On -:cp of the firet L.O.
co,.@!d be @-_ontin-_iou_zly -cu:_=d with-'n t 31.2 Xcls. For calibraticn pur-
poses, when a %,@nder-pouas:and ;.s required, @he second amplifier Iass
band could be swit@:hea _f'_-,Lr, 2 '.o 10 Kc/s wi-.hout affecting -.uning
and gain. The signal, dei-cted by a synchronoas detector, was iuken
from an R0 outp--i'?, :'11-ter -iixh :ime constant- -c @ 26 see. TiIi, s -4a-
lue permits ac;UeY.L,-,j; -@hc requ_red fluc-tua-.ion sensi-,.ivituy and in
practive does no: affe-.t - he ;.nterfference am.--itutle. All power 6up-
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S/169/6-1/006/009/001/018
Radioastronomical observations ... D2011D302
plies were stabilized with a stabilizati,.)n factor of about 103. The
signals were recorded on electronic automatic recorders type Ma-9
(EPP-0@) monitored by one minute time markers. The experimental da-
ta of'the receiver sensitivity are tabulated. The experimental sen-
sitivity was about half that calculated from Eq. (7). The maximum
sensitivity Of the interferometer, corresponding to the minimum
detected power levels, are also tabulated. In making final adjust-
ments (M.V. Gorelova particiRated in the final adjustment method
evaluation) constant and timevarying parameters had to be conside-
red. The constant parameters are y - angle between the horizontal
plane and the projec-tion of the base onto a vertical east-west pla-
ne, 9 - angle between the east-west direction and projection of
the base onto a horizontal plane and D - e of the interferome-
ter distance between the antennae*P'l- are delprmined by fixea antenna
geometry: @ = ff)n/X on the ot4er hand :.s determined by electrical
lengths of the cables and phase charactel-ist--ce of Input stages
and can vary with time. A geodesical survey gave the following re-
sults: D = 175.896 m; 21044 1@ 0 Al so that the exp.res@,,iinn Ix
Card 5/7

S/-@09/6VO06/009/00-/018
Radioastronomical observations ... D20-,/D302
for the azimuth of the source is given by
A - 1790461 - a r@ ui nf Q-0-0--V-Q-06n
S Ln Z k." 0 N'
- 0.047669 c-.g zJ,
where n - is the number of the lobe and z the zenith angle of
the sou"e. The parlamet-r - was determined from
L
tr tA 8ource
where T - the periodtf the interferen::e '.-ob-_--, t he calculated
r
and tA source - the real instant at which the sour-,e passes throt*#
the maximum of the interferenze diagram. Owing to the finite value
of the output cct time constant, the instant - at which
'A source
the source crosses the maximum of the diagram does notftrrespond
with t representing the maximum deflection of the seconding instra-
Card 6/7
20J'c18
S/109/61/006/009/001/o18
Radioastronomical observations D201/002
ment. L T thus was introduced, as given by
AT = t t = T(1 _ A_@ (I)2it (i2)
A Ascurce 3 T
in adjusting the arrangement* The above VAstrument and method of
observations were applied to .3 tracking the first, second and third
Soviet- space rocketsp launched January 2# September 12, and Octo-
ber 4, 1959, respectively; measuring their angular coordinates and
measurements of the intensity of the received signal were also
carried out. There are 8 figures tables and 11 references: 5 Sov-
iet-bloc and 6 non-Soviet-bloc. T e references to the
English-language publications read as follows: @ most recent
G@ Fielder. Nature,
19609 185, 4705, 11; H.P. Wilkinsp Nature, 1959, 184, 4685. 502;
P. Moore, Nature, 1959, 184, 4085, 502; J.G. Davies, A.G.B. Lovell,
Nature, 1959, 194, 468;, 501,
ASSOCIATION: Fizzi-cheskly Instilut im. P.N. Lebeceva AN SSSF (insti-
tute of Plivsizs im. P@N. Lebedev, AS USSR)
SUBMITTED: October 4,'1q6r,
Card 7/7 X

SOROCIfF,,;Ko, !1.1.
Radir) astronomical research and instruments. Vest. AN SSSR 31
no.11:88-93 14 161. WRA, 14:11)
(Radio astrono.V--Congresses)

luAwtihaLul Alim,
preliminazy results of observations 'dn the wave @jff 21 cm. of a
Milky Way region vith the center kz 20bl8m., (@'w 4V 301 * As tron. shur *
38 no.3:478-482 W-je 161. (KEU 14 a 6)
1. Fizicheskiy institut imeni. P.N.Lebedeva AN SSSR,
(Milky Way)

Q1 ;FO4/62/017/000/004/0011
104611246
AVAIORS: Sorochenko, R.L. and Ariakin, V.I.
MILO; Opace distribution of neutral hydrogen in Cygnus
SOUCE: idtademiyu nauk UZR. Fi;;icheakiy institut. Trudy, v. 17. ?Ioacow,1962.
Hadioa.stronomiya, 115-127
TUXT: The work refers @o the 21 cm radinmeal3urec,@nts in the area defined by
20hOO -,-' 0( ,, 20NO and 3bo z*rs represents considerai.,le '-A'iffi-
culti-o. Tht@ anoun'.. of orcanic subst.-tnee @v the ore
-,@wi not . )f. -ntirp hu e rses of
si -icient to transform the a
iron oxide material into a fe'rrous o:,Ide stiste. Tt orl:. suf-
fi,@rd to orwure t@e reduction of ea2ily redncible iron, oxide
und-Ir the formation of chamoisite, that -i!, to ray of CA-
Joid massej of iron oxide, rhich penetrated the fine -ehInD, -
quartz-like ore substrate. As regards the stxzge of formation
C.'ard of the ore deposita it c-in be maintuinedv thnt in PlIrticular

2o-4-52/67
The ?.Aticralogy and the Conditionn of Formation of the 1"arl-Green Iron (Tes
of Rorcbl
their hiph concentration 18 due to the activity of the rurf.
There rjre 2 fipures, I tnble, and IP referencets, 11 of
thich are Soviot.
AS-, -)C 1AT ION i(oF3to,.,ski.,,-n:,.-..,oru gov-iidnr@.,tvmnyi. univerl-it-It
4'ioetuv-m%-Donu .-Aitte"Univer-i'Aty)
?"j,..j;1T!@ D&*nuury 17, 1958, ny N. @-. @:trvkhov, Academy of
.'@ciencez, Ui"A
SUBMITTV,D: January 15, 1958
1. Iron ores--Geology 2. Iron ores--Properties 3. Iron ores
---Structural analysis 4. Iron ores--Materials
@7ard 3/5

-SCROCHINSKIY. A.F., kmadidat weditzinskikh nauk (Stavropoll); KVITASH, T.A.
.UP IGORTSIV, S.D. (Stavropol').
Discontinuous sloop and local therapy of certain skin diseases.
Vest. ion. i dorm. uo.@!51 My-JO 154.
(SKIN-I)IS]"as) (BLUP--THnAPZUTIG VSX)
I.-

SCROCHIIISKIY, A.F., podpolkovnik med.aluzhby, kand.med.nauk
I
Use of sloop In some skin diseases. Voen.-med,shtir. nO.12i8i D'55
(MMA 1211)
(SKIN-DISSAM)
(BLXZP-MMAPBUTIC UV)

GALOPHRIN. Abram Isayevich; NIKOUNKO. Viktor Filippovich: AQjO(ZINSIgY.__
A.M., red.; GALMICIWOVA, Te*N.t takhn.red.
[Transportation or long items] Perevosks dlinomernykh gruzov. Moskva,
Houchno-takhn.isd-vo 9-ya sytonobillnogo transp. i-shossainykh dorog
RSM, 1960. 50 p. (KM 14:1)
(Transportation)

ACC NRt 626@/6_@/660/001/0060/606@_,'
AP700611b SOURCE CODE: UA/
AUTHORS: Snitkovskiy, A. (Candidate of geographical sciences); Sorochinakiy,, X,
(Candidate of geographical sciences)j Pshenichnerj B,
ORG: none
TITLE: The satellite searches for hurricanes
SOURM Aviatsiya i koamonavtikap no. 1, 1967, 60-63
Z.ON 0 /?,go C E
TOPIC TAGS: meteorologic satellite,,weather forecasting, storm, heat radiation,
meteorologic research facility
ABSTRACT: Meteorologic satellites are put into orbits of 600--800 km to relay
information and advance warning on the formation and location of hurricanes and
cyclones. The satellites also relay information on the distribution of solar energy
for long-range weather forecasting and on the distribution of the ultraviolet sector
of the solar spectrum for determining ozone content and for studying the optic
properties of the atmosphere. Kosmos-122 measures atmospheric radiation,, ra,'-'
from the earth, elements of radiation balance, and radiation in ranges
microns and 8-12 microns. Cameras on board take infrared pictures on day and.night
sides of the earth. Computers reduce the data for a global chart showing distribution.
of radiation intensity. Plans call for launching additional weather satellites which
Card

ACC NRi AP7006118
can bo manouvered to designatod positions Vy signals (Folet-1 and Polot-2). Orig,
art. hast 1 sketoh and 1 photograph.
SUB CODEs22AO4/ SUBM DATSa' none
LCard 212

DEGTi,;V . G, F. ; SAVICHP T. V@ I SOROCIIIIISKIY Y. R.A.
Mechanized painting of metal articles. Mashinoatroenio no*3:8143
Mly-Je @ 62. (MIRA 15:7)
1. Dmpropetrovskiy inzhenerno-stroitellnyy institut,
(Painting, Industrial--Equipment and supplies)

DEGTEV, G.F.; SAVICH, V.V.; SOROCIIINSKIY, M.A.
Automatic painting and fryIng of parts. Mashinostroitell no.6s
15-16 Je 162. (MIRA 160)
(Paintingo IndustrW--Equipment and supplies)

I %V,f-!r I!. IT
:, n I k ;:. I . 7; . 1,@ i. 11,
, 1. r.0
i I
.-Trii- drive fr;r paintirg in an el,@.ctrlc fie'Id. MarhinogLrol tell
r.c.. 1. 28 ja 165. OMM@ 18:3)

SOROCHINSKIY, M.A.
Changes of jet streams in conrection wIth the development of cyclones
on February 13-17, 1962. Meteor.i.gidrol. no.9:24-31 S 163.
WRA 16.-io)
1. TSentrallnyy institut prognozov.

SOROCHINSKIY, M.A.
On the tracks of a hurricane. Priroda 53 no.3:118-120 164.
(MIRA 17%4)
1. TSentrallnyy institut propmozov, Moskva.

ar
L s4034_65
ACCESSION M. AT5W9165 0/0000/64/000/000/005210060
Aurwiti SoMbinskLZi N
+1
TITLE: Pressure changes due to geostrophic and actual relative vorticity
SOMCK: AN Uz9SR. Institut natematiki. ChLolennyye matody prognosa pogody I
Voprosy sinopticheakoy meteocologii (Numerical methods of weather forec*isting
and problems to synoptic meteorology). Tashkent, lid-vo Nauka Uz$SR, 1964, 52-60_._,-
TOPIC TAGS: geostrophic vorticity, real relative vortiefty, atmospheric pressures
numerical forecasting
ABSTRACT: The quasi-geostrophicity-principle -is widely-used during the develop--
ment of methods for nmerical weather forecasting. However, In nature, the air
particles Are not always in equilibrium and the real wind is often significantl7l
different from its geostrophic counterpart. The author compares the values of
the aciual (January and July of 1960) and geostrophic vorticities at the 300 mb
level above the surface centers of @Yclones over the entire period of their exis-;,
'tence. (A'similar study was made earlier by R. Z. Pettersen fi. of Hateorol.,',
no. 4, 19k77'at the tOO ob level.) He also analyzed Oressure changes at the
300 mb level due to vortex advection during the antics developeent of the cyo@tonaoj,@!@-"
The correlation coefficient-of.this study was somewhat smaller than the one
CGrd

1 54034-65
NF,
ON NR: ATS009165
bcained by Pettersen. The VIMSUltS 3how.that: 1) 'the difference between the
0
actual and geostrophic vorticity to approximately 44%; 2) tfie mean.square vorti
-city error from. pilot- ba-Roo n data- to __ half - the-correspondbig- geostco ror;
_phic er
3) the correlation between'the'true and calculated pressure change to very
However, pressure changes due to the vortex component calculated from pilot bal-
loon data are much closer to the true ones than the quantities obtained from thi
Liplacian of the pressure; and 4)'the targest deviations between the calculated
and actual ressurd changes are'observed in stage 11 when the cyclone is below .:he@
high fronM zone containing the largest ;@epptrophlc components. Orig. Irt# hass
1.6. formulas and 4 tables.
ASSOCIATION; none
CU...OO
SU34ITTED: -140ct64 IN SUB CM: KS
_j
WO RU SOVt 003 d
OTIMR I 001@
Card 2/2

.988-65 EVIT(I)/FCC AEDC.(a)/iSD(a)-5 GW
L 29
ACCESSION NR: AP5001816 S/0050/65/000/001/0040/0045
13
AUTHORS: SorochinskjX, M, A.
Z
TITLEi Dependence of the intensity of near-earth cyclogenesis on the kinetic
energy flux at the level of maximum. wind-
SOURCE: Moteorologiya I gidrologiya, no. 1, 1965# 40-45
TOPIC TAGS: cyclone, energy distributionp jet stream\-/
ABSTRACT: Since the maximum wAnd velocity changes considerab3,v alone the vorti-
cal, it should be proper to consider the kinetic energy reserves in 4he t
stream, not at the -isobazic 300-.mb- surfam (or at any- other such- surfacojebut
the level of =ximum wind velocity. The author traces the change in kinetic en-
ergy flux at this level for a period beginning 24 hours before cyclogenesis and
ending with full generation of the cyclone. He-plots the changes In kinetic on-
ergy during this period and points out that an investigations show cyclog)neois
to be accompanied by air-ilar changes in kinetic energy at the level of maximum
wind velocity. The energy begins to increase 12-18 hours before formation of the
cyclone and reaches a maximum at the instant of complete formation. With Growth
of the cyclonep the kinetic energy decreases, and a maximum is reached at
Card 1/2

L 29988-65
ACCESSION NR: AP5=816
greatest development (maximl Laplacian near-surface pressure), The author0o
4mrov+4rm*4-v% ol%-cro +Uft+ a m.ir I-- @--4--A -- 4-1- .-IA .4A. -P 4-U- 4-4.

7 tT 'I *i';-. e
"Witt ip" 711,

'ACC NR,-AT6032989 -__
SOURCE CODE: UR/2546/66/000/149/0092/0096
AUTHOR: Sorochinskiy, M. A.
ORG: none
TITLE: Slope of the maximum wind surface
SOURCE: Moscow. Tsentrallnyy institut prognozov. Trudy, no. 149, 1966. Rezul'tat
ispytaniy razlichnykh sposobov kratkoarochnykh prognozov pogody (Results of analyses
of various short-range weather forecasting methods), 92-96
TOPIC TAGS: maximum wind level, jet stream, wind speed, cyclogenesis, ageostrophic
wind .1 cv'r^-'@o C_
ABSTRACD. Although the angle of slope of the maximum wind surface to the
horizon 0 is very smalli it plays an important role in the develop-
ment of atmospheric processes, especially in jet-stream development*
Analysis of 100 profiles of maximum wind levels (vertical sections
through the center of a cyclone in the direction of flow) showed
that prior to cyclone formation, the surface-level cyclonic dis-
turbance was beneath the ribing branch of the jet-stream axis, and
in the period from its formation to the maximum development
stagel it was beneath the descending branch of the axis. This
indicates-thAt thereis a connection between*change@ @!j "o slope

'!ACC NR, AT6032989
AUTHOR: Sorachinskiy, 14. A.
ORG; none
UR/2546/66/000/149/0092/0096
SOURCE CODE:
TITLE: Slope of the maximum wind surface
SOURCE: Moscow. Tsentral'nyy institut prognozo Trudy, no. 149, 1966. Rezul'tat)
ispytaniy razlichnykh sposobov kratkosrochnykh prognozov pogody (Results of analyses
of various short-range weather forecasting methods), 92-96
TOPIC TAGS: maximum wind level, jet stream, wind speed, cyclogenesis, ageostrophic
wind cu/A-@o
ABSTRACT: Although the angle of slope of the maximum wind surface to the
horizon 0 is very small-, it plays an important role in the develop-
ment of atmospheric processes, especially in jet-stream development.
Analysis of 100 profiles of maximum wind levels (vertical sections
through the center of a cyclone in the direction of flow) showed
that prior to cyclone formation, the surface-level cyclonic dis-
turbance was beneath the rising branch of the jet-stream axis, and
in the pevlod from Its formation to the maxim= development
stage, it was beneath the descending branch of the axis. This
indicates that there is a connection between changes in the slope
Cqro 2@
L - __LL

ACC NRs AT6032989
SUB CODE:
angle of a jet stream and the rate of ground-level cyclone forma-
tion.
Results obtained indicate that the angle of slope 0 is affected
only by accelerations in the direction of flow; prior to the forma-
tion of a cyclone, there is a continuous buildup of kinetic
energy at the maximum wind level; and this contributes to the
development of ground-level disturbances-into a cyclone. After
the cyclone has formed, the kinetic energy of the jet stream is
spent in maintaining the cyclone formation, and the total kinetic
enp.rgy of the maximum wind layer decreases. When-the cyclone reach*a
its maximum, the kinetic energy on the maximum wind level increases
since the thermobaric field no longer contributes to further
development of the cyclone. Ultimately, the'situation returns to
one similar to that*existing prior to the formation of the cyclone.
Thus, surface cyclone formation involves reorganization of the
Jet-stream system, after which the disturbed equilibrium is
.-50;
restored. WA
04/ SUBM DATE: none/ ORTG REF: 001/
LCord_ 2L2

ACC W
AR6035262 SOURCE CODE.4 UR/0169/66/000/009/BO231BO23
AUTHOR: Sorochinskiy, M. A.
TITLE: Maximum wind surface inclination angle
SOURCE: Ref. zh. Geofizika, Abs. 9BI61
REF SOURCE: Tr. Tsentr. in-ta Prognozov, vyp. 149, 1966, 92-96
TOPIC TAGS: wind velocity, jet stream, wind, maximum wind inclination angle,
wind surface Inclination angle, inclination angle, cyclogenesis, surface boundary
layer
ABSTRACT: An analysis to made of the incline of tne surface of maximum wind to
the horizon, variations in the angle of inclination as a function of variations in wind
velocity components, and the relationship between the angle of Inclination of a jet
stream and cyclogenesis in the surface boundary layer. [Translation of abstract]
(SP)
SUB CODE: Vi
UDC: 551. 553

SOROCHIIISKIY. TS.M.
Significance of slow and controlled pneumoencephalography in the
diagnosis of cerebral tumors. Top.neirokhIr. 20 no-317-12 156.
(M1M 9:8)
1. Iz otdola neyrorentgenologii Nauchno-iseledovatellskogo instituta
neyrokhirurgii Hinisterstva, zdravookhrananiya USSR.
(BRAM, neoplasms
diag.. pneumooncophalographv)

GWHISKAN, Ta.l., prof.; SOROCRINSIU, TS.H.; TANANATKO, P.G.
Delayed and controlled pneumooncephalography in subtentorial
tumors [with summary in English. P-54]. Vop.neirokhir. 22
no.6:3-7 N-D '58- (MIRA 12:2)
1. Ukrainakly nauchno-issledovateliekly ins-4-itut neyrokhirurgiis
(BRAIN NEOPLASMS, diagnosis,
subtentorial, pneumo@-encephalogrsphy (Rue))

SOROCHINS4IY,_TP.@;t
.................................... I'--
Pneumoencephalographic peculiarities of extracerebral and intra-
cerebral tumors. Probl.neirokhir. 4:149-159 1590 (MIRL 13:11)
(ENCEPHALOGRAPHY) -
(BRAIN--rJNM)

GRYNTSM&N, la.I., prof.; SOROCHINSKIY, TS.H.; DANIIMO, G.S.
Graniography in the diagnosis of brain tumors. Vrach.delo no.8:809-
813 Ag '59- (MIRA l2tl2)
1. Otdol neyrorentganologii (zav. - prof. Ya.r. Geynisman) Ukrainskogo
instituta neyrokhirurgii.
(BRAIN--TUMORS) (MaJLI,-RADIOGRAPHY)

@-, t HTN-KiY, T-1. MI.
. ;
Cand Med Sci - (diss) "Retarded and direct pneumoencephalography
in turtiors of the cerebral hemiSDhere." Kiev, 1961. 14 jDp;
(Ministry of Public Health Ukrainian SSR, Crimean State Med Inst
imeni I. V. Stalin); 200 CODies; free; (KL, 6-61 sup, 240)

SUHOCHIbl4u.-Y,@, @
The working capital of collective farms. Den.i kred. 14 no.2:
22-25 F '56. (KM 9:5)
(Collective farms--Yinance)