SCIENTIFIC ABSTRACT RASSUDOV, N.S. - RASTAK, E.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001344230005-9
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: January 3, 2017
• Document Release Date: August 1, 2000
• Sequence Number: 5
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

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AUT HORS V Rassudova . G.N.,:Garas imov, F.M.,
'riTLt
_ThC u'so of'reflecting,,d ffraction gratings in
interference systaims:for'measuring linear shifts.,II
PERK-ODI-CAL., Optika -i spektroskopiya, v~,14, no.11, 1963, 559-563
Or
d,.EXT::,''~ The resultjs~are described of-an experimental investigation
,,o,f-`three variants of interference'systems using reflection and
.~trAns.mission gratings and.also-for-twb.-systems usin,3 reflection
4ira.tin gs.~ one with a half-, silvered mirror.and the . other a
Wo Ilai3ton. prism. as a- beam divider. A,bomparison is made of the
q.,,propertiels:of those'.systcms._~ It.is shown that they each
,cover.a Limited range'and.that, in-,this.respect they Are
-C omp... amen iii ry to each~ oth6r.-"., -These limits Are connected with
differe-nces'in dependence Of-.:the' banid contrast on distance between
the-Aratinss ' tho angular. size, of ,the source And the width of the
lk&~610ngth_range used. '.The merit of the different systems within
.:~limits,.of*,tlioir.applicabilitk..lies'.in the value of the bands
rathor.`.thdn.in the resulting light fluxes. The systems using
r0flocting graXings can.only,bo effectively used for obtaining
Card
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RASSUDOV,.S. M.
7
tkedieilnle.-,.~ ParatyAoid
Noy 53
"Experimental Reproduction of Septic Paratyphoid B,
Inf6ctibn in White Mice," V.,V. Akimovich) S. M.
Rassudw, Chair of 14icrobiol,, Saratov Med Inst
Zhur'Mikro),Epid, i I-min No 3.1, pp 46751
In order to bring about a lethal septic paratyphoid,
B infection in white mice, which normally are not
susceptible to this disease., huge doses.'of bacteria
are required'. These doses can be considerably re-
duc'ed. by using-bacteria which are in the lag-phase
(phase of.delayed multiplication) or J~y adynin-iste'r-
ing at the sametime agents which induce inflamms-
"tion in the MiN036.
2"2

0
124-57- 1- 86fj
Translation from:. Referativnyy zhurnal, Mekhanika, 1957, Nr 1, p 116 (USSR)
AUTHOR: Rassudov, V. M.-
TITLE: The Stress ed and Deformed State of a Slanted Orthotropous
Shell Reinforced by Stiffening Ribs (Napryazhennoye i
deformirovannoye sostoyaniye pologoy ortotropnoy obolochki,
podkreplennoy rebrami zhestkosti)
PERIODICAL: Nauch. yezhegodnik za 1954 g. Saratovsk. un-t, Saratov,
19551' pp, 688-689
ABSTRACT: Examination ofthe flexure of a thin slanting orthotropous
shell, having a rectangular planform, reinforced by stiffening
ribs. The shell is bent by anormal pressure, distributed
over the surface of the shell. Differential equations are
adduced for the deflection of the shell and the stress function;
the bounda-ry conditions for the integration. of these equations
are also shown.
l., Shells--Stresses--Mathematical analysis Ye. F. Burmistrov.
2 Shells--Deflectioz,~--f4athematical analysis 3. Shells--Theory
Card 1/1 4* Differential equations--Applications

7m~lff
SOV/124-57-4-4609
Deformation of Shallow Shells Reinforced With St'ffeijer Ribs
2
2,
V
+
7y k 2 2
Jx R ax R ay
where E is Young's modulus, D the cyll',ndrical-st'ffness, v the Poisson ratio,
:~'h the thickness of the shell, F(I 6 nd R'> the p-:yicpal'radIi of curvature, qj the, load-
-ing distributed over the various regions of the sheil, and (P the func'tion sought in
terms of which all desired values ate expres5ed. The solution of equation (1) is
given for a shallow shell, two edges of wh~:ch are freely supported while the other
two may be fixed Jn any a rb- tra ry manner. TLe solutxn is found 'r the form of the,
series
kv
y (2)
ik,x) si n
The author then examines the deformation of a shallow cylindrical arched roof -rein-,:
:forced by n rectilinear rib stiffeners. He then the differential equations
for a shallow cylindrical arched roof !einforced by a 5in8le rectilinear rib stiffener
and s b'ected to a normal, uniformly distributed, pressure force acting in
Card u2y3

24~' ~Detorustion of Shallow Shells Reinforced by Rixid-Ribs
"Deformation of Shallow Shells Reinforced by Rigid Ribs#" by
V. M. Rasoudov, Uch. zap. Saratovsk. un-t, 1956, 52, PP 51-91,
Cf-r a-R-ere_r_af1vnyy Zhurnal -- Mekhanika, No 4, Apr 57, Ab -
stract No 46 by B. F. Burmistrov)
"This article contains an Investigation of shallow isotropic shells
Indluding those of zero Gauss curvature, both reinforced by rigid ribs.
"The variation.method is used to obtain the basic differential equa-
t1ons and their relationships with the theory of shallow shells of given
foms and with rigid ribs.
The derivation is given for the basic diVerential equations and the
bowdary conditions of the rigid ribs during conditions of small defor-
.*Ations. The obtained system:of equationsboile down in the beginning
system of two equations for tbefunctions.6f stresses and the func-
tions of,bending and afterward to one equation of the eighth order in the
fo.me

kIr
sin- Y.,
W
b (2)
k I
"Afterward, the deformations of a shallow cylindrical arch rein-
"..:forced by nrectilinear rigid ribs are described. Later, the integra-
tions of the differential equations for a shallov cylindrical sbe*.l --,;ith
rectilinear rigid rib are performed for the case of a normal uni-
formly distributed pressure, under certain conditions, on the sides of
the shell. The case is studied in detail vhere all sides of the shell
r*st freely on roller bearings. Also given are the rical values of
bending, the norml stresses, and the bending moments for certain ratio@
of g/h. vbere g is the rise of the shel.1 in the center.
"A method is described for the solution of the problem of the defor-
vAtion of a shallow cylindrical arch resting freely on all sides and re-
inforced by rectilinear ribs, vbieh reduces.the calculations to the solu-
tion of a beterogenous linear algebraic system of four equations With
four un)movnz."
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2zq4), 24(7) SOV/51 -k;-6-29/34.
AtMORS Ras"Ic-m, G.N, and Ger.asim,;T, F*Mv
TITLIt Diffiaction Gratingi for ^eparation of Spectral 0.
rerhatVI dlys razdoleniya poryadicov spelctra)
FERI 001 CAL iOptika i apeIctrcRkc,VIya, 1-959, Vt.I 6, Nr 6, pp e2ti-927 (USSR'
ABSTRACTs The authore prepared special reflection gratings *Ich could be vEe~ to
separate apectra of variovF crders prcd,~~-eAl by other diffrac-tion
gratings with any -number of line,; per =. These reflef.,tion gratings
(separator-grat!.agi) had 50 or 100 linea/=. Thair lino profile, wa.3
stt%p-lilce with -morkIng vu.-Tavms inalLvA, at 10 to the original surfa-:%
Im order to .,on,,.i,,jtrate llg~%t ir. the first erder. Tna separator
gratingg were with other gratings (uzed at diffrattion angloji
of 40-500) an4 tested in an wato--,mlliwating, spectrograpla w-Ith f - 3 m,
A parallel boom rea*aad a e6parator-&-.uting (vhleh va5 riorircutal)
iaakmng an angle of with the plane parallel to the line.* ca thi;
gratinS. After diffraction frum the main grating (whoss lines wers
vertical) tbs been 7~eaahel, the, 5eparator gratin&i for the so-O.Y.A. tjmw and
then paa s ad va tc~ an o~-j e itt v-. U.-4er tno:;e ~ondltionn multIpIlt
diffraction of b^.um vava-~rc-Ldee. '-'-.zt veak sOlditional iin,~-q appAarFO
due to neighbott--ing oL-),%rv of the -nerarat, :--gratini
g. Spel,,tral rep on
of the order of 112 oota-~f, bota In two visible aryl' ultraviolet regiow,
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_7 77

AUTHORS: Sapgir, I 'Hassudova, N. S. 64-6-17/19
TITLE: P. M. Luklyanov. History of the Chemical Profession and the
Chemical Industry in Russia (P. Lt. Luklyanov. Istoriya
khimicheskikh promyslovJ khimicheskoy promyshlennosti
~PERIODICAL: Khimicheskaya Promyshlennost', 1957, Vr 8, ppe 52-52 (USSR)
ABSTRACT: This is volume.number 4. Under the editorship of
S. I. Vollfkovich, member of the Academy. PublishinC house,of
the Academy~of Science USSR, 1955. 622 pages. The book is here
discussed in short. This volume is entirely Civen to the
history of the production of dyes in Russia from ancient,times
up to the begin of the 20th century. A great number of
oriCinal documents,.manuscripts, etc. are given. A great part
deals with the investigation of fre3co-paintings, miniatures,
and icons. The author procured, often with great difficulties,
small quantities of these old dyes and investigated them by
means of the spectral analysis. The results are comprised
in a table.,The fresco-paintines, miniatures, and icons are
contained in the book in good reproduction. The book is
well-written, and contains a detailed name-, subject-,
Card 1/2

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SOV/24-5 -4-6/33
9
AUTHORSt Moskvitizk. A.I. and Rassulov. A.M0 (Moscow)

TITL9f ~~'Pin the Hydrogen Cooling System
Concerning Heat Tran;i`or
of Turbo-alternators~,A
PERIODICAL : Izvestiya Akademii nauk SSSR, Otdeleniye tekhnichookikh
nauk, Energetika i avtomatika, 1959, Nr 4, pp 43 - 48 (USSR)
ABSTRACT: In modern turbo-alternators gas coolers are used to coal
the circulating hydrogen; these coolers.are.yery big and
can have a considerable influence on the design and overall
dimensions of the alternators. It is.ijuportant to be able
to make these gas coolers small. However, heat tran for
and the aerodynamic resistance of bundles of tubes with
wire ribbing has been little studied and published data
relates only to tests in air. In the summer of 1958, the
Energeticheskiy institut AN SSSR (Power Institute of the.
Ac.Sc.USSR) together with the "Elektrosilail Works made min
anexperimental study at various hydrogen pressures of heat
t anAfer and resistance to,flow of gas coolers with wire
ribbing as xised in turbo-alternators. As the tube bundles
Cardl/6 were of fulLsize and the cooling medium was the same as
.4;

Zi!' N *,.'x ~4 -I
';9 ~.Mt~_W_Ixmny

sov/24 9-44/33
6acerning Heat Transfer in the Hydrogen CooT~ing ystem of
Turbo-41teknatorz
in.operatiotL it was possible to determine the heat-transfer
coefficient and resistance at various hydrogen pressures
also to obtain generalised criterial relatLonshAps.
The tests were made in special equipment designed for
testing.parts of large machines in an atmosphere of
hydrogen at pressures of I to 10 atmi it Is acylindrical
chamber 5 300-mm: long and 1 050 mm,diameter. The chamber
contains a wind tunnel with:fans forming a closed circuit
in which the gas can be circulated in amounts up to
1.5 m3/sec. Appropriate control measurement devices were
provided. The tests were made at various hydrogen pressures
from 1.2 to 7.5 atm,and for a wide range of gas speeds from
2to 10 m/se% The gas temperature at inlet to the coolers
0
reached 50 0 C and the cooling-water temperature was
around 20 C.. During the tests the thermal loading of the-
gas cooler corresponded to practical operating conditions
and was 800 - 1 200.kcal/h per metre run of tube. Hydrogen
of 97.5 - 98.5% purity was used as in practical.machines.
Card 2/6
1r
:r
M

SOV/24-59-4-6/33
-Concerning Heat Transfer in the Hydrogen Cooling System of
Turbo-alternatorx
Heat transfer from a ribbed gas cooler is given by Formsl&
(1) and the efficiency of the ribbing is given by Formula (2).
Using these formulae, by experimental determinations of the
amount of heat,tranatrred.and the appropriate temperature
drop it is easy to determine the heat-transfer coefficients
for the ribbed surface. On going over from air to hydrogen
cooling at a pressure.of 4 atm, the effectiveness of usiLng
the gas coolv is reduced by about 20% and, therefore, with
hydrogen cooling at 4 atm, It is advisable to use wire
ribbing with a larger wire diameter and smaller loop height
or to use solid fins. The criterial heat-transfer relation-
ship of the gas cooler plotted in Figure I and given by
expression (4) was plotted from experimental data for
hydrogen pressures from 1.2 to 7*5 atm.
The aerodynamic resistance of the tube bundle is then
considered. The criterial equation for the resistance is
of the form of expression (7). On working out the
experimental data, it is found that the resistance
Card 3/6
W~

SOV12 3
,Concerning Heat Transfer the Hydrogen 00~~n'j_'~_y'slt'em of
Turbo-alternators
coefficient drops as the hydrogen pressure.is increased,
for instancet' on raising the hydrogen pressure from 1.2
to 4.0 atm, the resistance coefficient drops by 15-20%
for a rate of flow of 3.0 a/sec. Figure 2 shows a graph
of the criterial relationship between the resistance
coefficient obtained on tests for several hydrogen pressures
and for air. It Is found.that whIlst 2ir increase In
the Reynolds nunber reduces the resistance coeffictent
onl)~ slightly, the reduction-iB greater for hydrogen and
increases as the pressure is dropped. On the basis of
the testresults, Eq (9) is recommended to determine the
res:Lstance coefficient.of the wire ribbed gas cooler
considered, it'a pressure of 4 atm. The tests also showed
that on going over from air to hydrogen cooling at a
pressure of 4 atm, the,resistance of the gas cooler is
more than nalved.
The experimental separation of the various components of
the thermal resistance of the gas cooler is then
4/6 considered. Sine ethe tests were made over a wide range of
Card,
xq,

SOV/24-59-4-6/33
Concerning Heat Transfer in the Hydrogen Cooling System of
Turbo-alternators
:speeds and gas pressures and of water speeds in the tubes,
it was possible to resolve the thermal resistance of the
gas coolerinto its,component parts and this is, of course,
a major object of investigations of heat-exchange equipment.
Of course, the resistances of the different parts are inter-
related so that the separation Is necessarily somewhat
arbItirary.
Figure 3 g:Lves graphs of'the total specific thermal
reststance of the~gas cooler as a function of the reciproaiL
of the water speed for tests in hydrogen amA.in air and
for various gas speeds and pressures. The relationship is
linear and the method.of using these results to resolve
the',heatlosses into various components is explained.
diagrams of the various components of resistance
percentage of the total resistance are plotted In Figure 4
and. JtLwill be seen that for air at low speeds (Figure 4a -
lefthand column) the main resistance (83%) is due to heat
transfer from -the gas to the ribbing. For hydrogen at high
Card5/6

SOV/24-59-~-6/33
,Concerning Heat Transfer in the Hydrogen Cooling System of
Turbo -&1t ernators
speeds and pressures (py 33, right-hand column of
Figure 4a) this resistane e drops to 25% but the relative
proportion due to the resistance of the metal increase:
considerably :rcow 89*' in'airto 50% in hydrogen. Con-
sequently, in this case, it Is best to make the rtbbln
narrower but of thicker wire. Formulae (10)-(12) may
be used for approximate recalculation of the test results
for the,given gas cooler from air to hydrogen and thus
to obtain a-generalised characteristic for the gas cooler.
Such a generallsed characteristic is given in Figure 5 for
the thermal resistance relating to a hydrogen pressure.of
atm and gas speed of 5 m/sec constructed from the test
results given in Figure 3for hydrogen and air#
There are 5 figures and 5Soviet references.
SUBMITTED: March 10, 1959
Card 6/6
lit"
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141
E 0 0 N -UM ph, L , 1 M

i 1M,-- , 1--i- i,
- 1. ---

VAGINA, V.S.; RASSULOVA, Kh.N.; DMIMIYEVY O.V.
Morbid states following resection of the stomach and their compound
treatment. Sbor. nauch. rab. vrach. san.-kur. uchr. profsoiuzov
no.1t98-1CV, 164, (MIRA 18:10)
~1. Zhelaznodorozhnyy bazovyy sanatoriy imeni XX s"yezda Kor=unistiche-
skoy partii Sovetskogo Soyuza (glavnyy vrach R.S.Chubarov, nauchnyy

85009
3/048/60/024/010/018/033
~,"/300 (11371113~01V3)~ B013/B063
AUTHORS: Bo danov, S. V. and Rassushin,__V. A.
of BaTiO
TITLE: The Semiconductor P, ]-xI-
PERIODICAL: Izvestiya Akademii nauk SSSR. Seriya fizicheskaya, 1960,
Vol. 24, No. 10, pp. 1247-1250
TEXT:' The authors studied the effect of.some slight additions to BaTiOx-
upon its semiconductor properties. Some data are given concerning the
dependence of log ?_on 1/T for BaT'03 monocrystals, to which linthanum
and vanadium were added. The crystals were bred according to the method
described by Remeika. On the introduction of additions the number of
lamella-bhaped crystals was reduced, and the principal mass was
granulated. In the case Of V205 the crystals were bright-yellow. With
La203 the color,varied between pink and violet. Regarding the addition
concentration in monocrystals, no precise values could be established. By
indirect values it is possible to estimate whether the addition is
contained in the crystal. Fig. 1 shows the temperature dependences of
'Card.1/3

85009
The Semiconductor Properties of BaTiO
3 S/048 60/024/010/018/033
B013/BO63
C for monocrystals with La and for BaT103. The temperature dependence of
resistivity was measured for the monocrystals obtained. Individual results
are given in Fig. 2 for crystals with vanadium. At room temperature,
resistivity amounts to 1.37-1012 ohm-cm. For specimens with lanthanum,
data are given in Fig, 3- It may be seen that there is an anomalous
section in the curve log T = f(I/T). This resembles the section described
by-Saburi for ceramic BaT'03 specimens with rare earths. Its existence can
likewise serve as indirect evidence of the presence of the addition in the
crystal. A great reduction of the quantity y could not be achieved.
Similar results were obtained on a large number of specimens. The
ano.malous course of the curve ?(T) can be explained by the fact that this
section lies in the region of the phase transition, during which a
rearrangement of the zonal crystal structure takes place (Ref. 12).
Below.the phase transition the additions are split, which fact leads to an
3.norease of conductivity. Above the phase transition splitting disappears
and conductivity is reduced. Mention is made of LT. D. Mashkovich, Ye. V.
Sinyakov, B. K. CherUy, A. F. Yatsenko. The present paper was read at the
Third Conference on Piezoelectricity, which took place in Moscow from
Card,2/3

-L 18949&2 LFWT I)JUP WT IM -2
SM Pt-4 GG/JD
ACCE SSION NR: AP3007316 S/0181/63/005/009/2703/2704
AUTHORt Boadanov,.S. V.;:Rassushin V, A.;,Sinkha, D. K.
"BMW OWN"
TITLEt Relaxation properties of UU03 s*ingle crystals containing t
antimony Impurities
S ums'4izika twerdogo tels. v. 5, no. 9, 1963, 2703-2704
~TMC TAGS: barium titaftate relaxation property, single crystal
P
barium titanate single crystal. barium
relaxatLon property,
tit nate-crystal property, ~bartun titanate crystal,, bartua
tLtsnote, relaxation property, barium titanate dielectric property
ABSTRAM The dielectric constant as a functLon..,of\temporaturo
was investigated In barium titanate single crystals7containinlt
Sb203 impurities. It was found that 1) the single crystals of
barium titanste possess ferroelectric and relaxation properties
for certain antimony Impurity concentrations; 2) the introduction
VWd 1/2

WCEWION UR: AP5004*,~
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Curr
L-51564-65- -,(S)-2/ (fia EC t_ /t/E~40(t)/SVP(b)/EWA(c) Pt-7/Pl-~
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NRV _1 5 00 94/09,98
.4cot'SSION
6/09

sx~off', sonas
-":Bogd h4MAX Ra
ssushin,
ina,NX0

.~,.TITM t eat -do
91

bin I ping ~jith'-- ipo on: some physical proj)erties of

& ^4nfpe COM
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All
Union vo
4th
fe
. -
rence on i
n
:Terroelec tr city held:in-Rostov-on- the-Don 12-1 8 �pDt__DGA/
SOUROE;-.AN.SSSR$Izvestiya~Ber'ofizi6he~ic6~a- v.29 n6.6, ~965, 994-998
-
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rABSTRACT.'''
.. The!':'aut ors ave;measured~the-dielectric..constantI elec-_
.

y--* -ion of -BaTiO,3
-and,-optIOal--.tran 5
ical - donduetivit smis _,singl
e C17s_
_
.t-ia- -
-and have--Ih i re.
t6L-Ang--up-to-.6~:at f.: Fe- -vest gated the structu
f t1i, tals'by ~c-ray., diffracti6n.-, At -room temperature- the struc---*
Vara',__6f crystals _.odi'ttaining., from -0-6'01~. to - 2*6 at.f. Fq w0-tetraZonal;
w
r
.~Crys_Uls -odntaining-m6m than,2,6-at- PO V are cubic -and their lat
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ACC NR- 026?16 SOURCE c6iff~-ffl&l-~-IT6 2--4-8*8-
/2490
AAUTHOR: Galkinas T. I.; Peninp N. A.; Rassushinj, V. A.
1ORG: Physics Institute im. P. N. labedev, All SSSR, Moscow (Fizichaskiy institut Mi-
SSSR)-
-.'JT1TLF,; Dater~mination of the energetic position of the acceptor level of cadnium in
Indium arsenide
SOURCES Fizika tverdogo telap v. 8 no. 89 1966, 2488-2490
TOPIC TAGS: arsenidep indium compound, cadmium, ionization
ABSTRAM, The ionization enorU ofcadmiun atoms in InAs was deter;Tdned from the spec'
tral. position of the recombination radiation line of indium arsenide diffusion diodes,.'.
1ho observations wrore made by transillumination
~hrouZh the n-rogion of the naterial
which had'an*'electron concentration no = 2 x 1010 cm7J. It is postulatedthat the
radiation of the diodes arises in the p-region due to radiative capture of an electrons
from the conduction zone by a neutral cadmium atom. In thia case, the spectral char-
acteristic of radiation for direct transitions between the conduction band and the ac-
ceptor level is expressed,by the formula
G(y) Y-1/2,yo
where Y- + (SU
and &-jis the energy of a radiation quantum, It follows that-
the.maximum ofltL radiation intensity lies at y 1/2, 1. at t"Max Cd 'a
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,~Cczrd " 1/2 ~ ~ I I- Ij . -
- 11 . UDG: Ul. J 14.:o I.
.j 7~~ - 4 , - ~ .1 1 - I .,
- - - , -,:, - . ~- , ., -1-

WA=
-66
L .16802
:'ACC M AP6005292
signal", cobalt-59 is used as the working medium in the resonance system* Orig# art. L
has- I"fiiure. [KM)
~:~WDE.--,-09/ SUBM DATE: 26Mar65/ ATD PRESS:
(P07
"SUB

UGLOV, F.G., prof.; WEDUV, I.M.; 'fjiaA-LOVA, R.A.; KRASNOSHCHEKOVA, L.I.;

USSR/MicrobioloMr - Microbiology ratlioCenic to Humane and F-4

Abe Jour Ref Zhur Biole, No 12, 1958, 529o6
Author Rasevotayev, VJ,
Inst
Title Intrauterin Fetal Infection by Tick Spirochaotes,
e

Orig Pub Za sots. zdravookhri Uzbekistana, 1956) No 6, 41-42.
Abstract Of 33 prognant women under observation 12 were treated
before delivery by miarsenol, 3by.streptomycin, 2 by
streptonycin and syntomycin, and 2 by biomycin. In 9
nmyborn infants whose mthers were not treated, spir-
chaetes were found in the blood. .11 wo=n who reccived'
lelivery (pvc birth to
1-2-1.5 a of miarsenol before d
healthy, uninfected children. Children born of nothers
treated by other methods proved to be infectec' by spiro-
chaetosis. Of all arsenic preparations, the most offec-,
tive in treating pregmat women ill with tick spirochae-

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USSR/Human and Animal Physiology - (normal and Pathologicnl). T
Physiology of Work and Sport. Aviation Physiology.
Abs Jour Ref Zhur Biol., No 4, 1959) 18033
Author Rassvetayev,LV.V.
Inst Military Medical Academy
Title Secretory and Motor Functions of the Stomach in Digs in
MotionSickness. (Experimental Investigation).
Orig Pub Tr. Voyen. -wmed. akad., 1957, 79, 5-50
Abstract No abstract.
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L n378-67
ACC Nito AT60363M
action. time of a reaction with choice, number of errors, amount of
Information processed. input (or traffic) capacity.. andlime required
'for processing one unit of information. It was found that the input
capacit of the visual analyzer increased gradually in the first 9 hr& of
y
flight, and then decreased by the 15th hr. However, the input capacity
of the auditory analyzer decreased regularly during thd entire.flight.
The input capacity of the tactile analyzer Increased (with some varia-
tions) until the 12th hr, and then decreased to initial levels..
acities observed In visual and
The gradual increase in input cap
tactile analyzers in the first 9-12 hre of flight is probably due to
!adaptation of the organism to new conditions, with increased analyzer
~ability. The subsequent decrease in input capacity in caused1by
fatigue, first noticed in crew commanders. 7`he high noise level in
the aircraft contributed strongly to the decrease in auditory analyzer
input capacity. Characteristically, the greatest shifts in auditory
function were observed in commanders and radio operators, who are I
responsible for external and internal radiocommunications. 71io
visual analyzer in kept in a tontinual state of stress by the MCOM41Y
'for constant monitoring of masW Instrument& In the auditory
`anabmw inhibite. d1eveloped"in the cortax due*
;7 processeer we
CWd 2/3
US:

L 11378-67
lmmrn~

-L 47224-66 PO
ACC NR, AP60224321 SOURCE CODE: CZ/0040/66/000/003/0061/0063
AUTHOR: Ra'sta'k, Eenjk
ORG: none
11V
TITLE:: The Z-37 Cmelak". [aircraft] and Its equipment for use in agriculture
SOURCE: Letecky obzor, no. 3.0 1966f 61-63
TOPIC TAGS: chemical spray tank agrictilture, utility aircraft, auxiliary aircraft
equiplitt-LI,t
;ABSTRACT: The article deacribes.the application of agricultural equipment used on the,
Z-37 Cmelak.'.. The mechanical transmission which powers the agricultural equip-
ment from t of,the aircraft. (output 12 HP at 2,0C0 rpm), the container of chc*
stainless steel.co'nes 670 dm3 ill Ivolume), and the applicatioii equipment
yer, spreader arative data for the out-
,(spra etc.) are described., A table gives, comp,
.puts of several types of agriculturataircraft (Z-37, L-60, JAK-12, and Piper Pawnee)J
The data refers to the operational speed, chemical carrying capacity, type of trans-
~mission and maximum output, and the width and volume of the spraying of grninulated,
The rotating spreaderi
ichemicals, dust chemica'ls,.waLer solutions, and oil solutions.
,of mineral fertilizer
s is a technical noveltywhich received a Czechoslovak patent.
!When adispersion wing is added to'the spreaderp the overall width of spraying can be!.-
.,.Ancreased to as much as 60 m. :.The output of the Z-37 Cmelal: Is almost twice as high
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