SCIENTIFIC ABSTRACT LIDMANOWSKI, W. - LIDOV, V. P.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R000929820017-3
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: January 3, 2017
• Document Release Date: July 31, 2000
• Sequence Number: 17
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

LIDMANOWSKI~ WACLAW
Technika. wysokich napiec. 2. wyd. Warszawa, Panstwowe Wydawn. Techniczne, 195h.
211 p. (High-tension electrical engineering. 2d ed. Mus., bibl,)
NN Not in DLC
SO: Monthly List of East European Accessions (EEAL) LC, Vol. 6, no. 7, July 1957. Uncl.

Routine tes ting of the Im3ul& tion for Id,-,i voltai-e p 2
PRI-CF vol. 4, no. 10, 1954
Warszawa, Poland
so. EI--;'T F-JK,',Fji"4 LIS Vol. 5, ac). 10 6ct.

LIDMANOWSKI, W.
First mobile laboratory for routine tasting of the insulation for
high voltage* p. 28*
FRACE, Vol. 4, No.-IO, 1954, Warsaw, Poland.
SO: East European Accessions List, Lib. of Cong., Vol. 5, No. 10j. Oat. 1956o

L . I IJKI, W., Rr"O, H.
Calculation of cross sections of conductor5 subject to heating by lightning
currents with consideration of their surfaco-s, n. 115. (Archii-rum Elo-ktro-
techniki, Vol. 6, No- 1. 1957, Warsaw, Poland)
SO: Monthly List of East European Accessions (EEAL) LC, Vol. 6, No. 8. Aug 1957. Uncl.
-P-0.

POIJUM/Optics - Instruments for Optical Analysis K-9
Abs Jour Ref Zhur - Fizika, ljo 1) 1959, No 2196
Author TAdmanowski Waclaw
Inst
Title Electric DIscharges Used in Spectral Analysis, and Methods
for Their Production.
Orig Pub Poruiary,, ailtomat., kontrola,, 1958) 4) No 4. 151-153
Abstract No abstract
Card 1/1

P/021/60/0w/w6/oo1/002
A105/AO26
AUTHORSt ~idmanowski, W.; Boguslawski, S.; CXranowicz,-K.j Fekecz, J.
TIM: Composition ana.Technology Tests of High-Voltage Porcelain V~
PERIODICALt Przeglgd Blektrotechniczny, 1960, No. 6, pp. 227 - 231
TOT: A brief description of tests for improvement of insulating porce-
lain performed in the Zaklad Wysokich Napiec (High-Voltage Section) of the Zak-
lad Materialoznawstwa Institutu. Elektrotechniki (Material Research Division of
the ElecLtrotechnical Institute) is given. ~The purpose was to find a porcelain
'body with better mechanical properties than required in Polish Standard PN-56/E-
-06301 and in German Standard DiN 4o685 (1957), listed in Table 1. The inflmme
of the porcelain-body composition on its properties is discussed and shown in 2
relation triangles (Figs. I and 4) introduced by G.J. Gilch-rest and T.A. Kline-
felter (Ref. 1) and by Wiedmann (Ref. 13), respectively. The influence of the
size of quartz granules in the porcelain body on its tensile strength is dis-
cussed and shown in 2 macrophotographs (Figs. 2 and 3). Mechanical properties
of No. 31, No. 32 and No. 5 porcelain bodies, which are being produced In an un-
specified Polish plant are given in Figure 5 and Table 11. There are 5 figures,
Card 1/2

LIDMANOWSKI W., mgr ins.
Shook resistance of insulators under rain. Przegl elaktrotech 38
no. f 62.
1. Kateora Wyookich Napiecs Politeohnikaf Warszawa.

LIDMANOWSKI, Vaclaw
Certain problems concerning surface discharges. Rozpr elektrotech
10 no.3043-359 164
1. Department of High Voltagess Technical University, Warsaw.

B. LID14M
"Treatment, storage, and conservation of eggs." p. 64. (VYZIVA LIDU, Vol. 8,
no. 4) Apr. 1Y.53, Praha, Czec-loslovakia.)
SO: Montnly List of East-Europe~an Accessions, L.C., Vol. 2 No. 7, July 1953, Uncl.

LIDMIL-'~, B.
Industrial production of eggs and poultry meat.
P. 402
Vol. 3. no. 5, 1955
SMIRENSKA VYROBA
Praha, Czechoslovakia
SO: Monthly List Of East European Accessions, (EEAL). LC, Vol. 5. no. 2
FebFmary 1956, Uncl.

LIDNILA, M.
Ion exchange in polarographio determination of lead in urine. Pracovni
lek. 4 no.3:221-234 June 1952. (GLKL 23:4)
1, Of the Institute of Industrial Medicine (Head--B. Sveatka, M.D.),
Kladne.

t f!~P
2
SOURCE: Elektrotekhnika, no- 3, 1965, 3-5
TOPIC TAGS: electrochem-la-try, acoustic transducer, acoustics
Abstract: The transducer with two-sided diaphragm (Fig. 10 is a plastic 7esnel
-omprl5ing two chambers com-ected by a chq~nrel
el

ACCESSION RR- AP5007530
.^-,-W _y-.Ow A4
e so=d pressure is evident in Figure 2b.
FIgure 2c shows the dependence of output current on SoUnd nresuure. 7~!C- Dr, n pal,
cYL,qrP,7tsr1et1cs of the acoustic ire R!~ af
ie~ends on soUnd n~P
Ara ZU P;;Lage __O k. Measurabl a-
400- istii3m = 1=1ftieffl-
, liuidiugf-t
4id dc transducer of emall meahaxdcaa
a aCeMent& is A plazitic vessel with two concentrically a_rranged c4aj7bers
"Fig. 20. It has a one-sided diaphragm arran~pene,-,,
-z:-. frequency i& shown in Fig. thp leperider-
stgna2 frequenc,, a' a
CA-,Age ~,ependa on the magnitude of
of meapurabla lispl acernerti3,
MV)
'Pro! 9.
T
M

1A
r X, olat -
p r.
tf; shcwr, ~~n, Fl.-, -'a.

A 1:'C097

Cf the
MVI
OR
U14

------------
_T,_3e,54h
;6
ACCES'71-OR '-IA: AP5008198 -3/(~,-96/65/000~00'=.,,'oo65/bo65
T'-'V Nablullin, F. Kh.: Lidorenaco, N. S.; Pentk-!--ra, L. F.; Slaik-v YI S
Byulletan' izobreteniy i tovarnykh znakov, no. 5. 1965, 'D5
7-7- ':A~;S: concentrator, radial enen~, , mqtal foil, m-irr.)r, '.-t,m, radia-
13nergy
This Author Corti-ficate jp~-~,iuces
saf la.~ 1,7-,
~'rodul ced cy Lr';; 1 e.3
-3 nz 7-.
thg Eipy. Ic a t ir: i c r) Ll

lfc cr ~lt-

L
ACC NR: APGO30579 SOURCE CODE! UR/0413/66/000/016/0058/0058
INVENTOR. -Kocherg1nBkiy, M. D. ; Nen1kova, L. F. ; Kalachev, S. L.
Lidorenko, N. S.
ORG: none L-?
TITLE: Rechargable disc shaped alkali,galvanic cell. Class 21, No. 184948.
[announced by 11-Union Scientific Research Instit 6urces,(Vsesoyuzn,
nauchno-issle=MNstitut istochnikov toka))
SOURCE: Izobretenlya, promyshlennyye obraztsy, tovarnyye znaki, no. 16, 1966,
58
TOPIC TAGS: galvanic cell, rechargable galvanic cell
ABSTRACT: An Author Certificate has been issued describing a rechargable
disc shaped, allcali- galvanic cell with a negative zinc electrode a positive manganesi
dioxide electrode and a thick electrolyte diaphragm (see Fig. 1). To improve the
electrical ratings, the cell is provided with a casing having a symmethrical lug
along the inside perimeter on which the diaphragms rest with the negative electrode
between them, while the positive electrodes are arranged above the diaphragm.
Card 1/2 UDC:-621-.352.-7

L 05795-67
AP6030579
Orig. art. has: I figure. [Translation]
.... ...
r C444~4~441j444j
Fig. 1. Rechargable alkali-galvanic cell.
1-Casing; 2-casing lug;
3-negative electrode; 4-
current lead; 5-casting compound;
6-diaphragm; 7-auxiliary
diaphragm; 8-positive electrode;
9-positive current lead;
10- depressions of positive current
lead; 11-plastic film.
SUB CODE: 09/ SUBM DATE: 03Jun65/
C.,6 2 / 2

ACC NR: AP60z9786 SOURCE CODE: iiii'o"119/66*/000/008/0005/0007
'AUTHOR; Belevtsev, A. T. (Candidate of technical ociences)l Voronkov, G. Y&.
.'(Gandidat6 of technical sciences); Lidorenko, N. S..JCorresponding member
.,,AN SSSR); Fedorin, V. A. Wnginee~r~
:ORG: none
i,nTLE*. Electrochemically-controlled resistor
:SOURCE., Priborostroyeniye, no. 8, 1966, 5-7
TO PIC TAGS- resistor. electrochemically controlled
tor
14
'ABSTRACT: The elecl ically-controlled resistor
,consists of cell I (see figure) filled with an electrolyte and
;containing resioti-~e electrode 2 and control metal electrode
3. D - c control signal to applied between one - end of 2 and 3.
:,Readout a-c signal appears between A and B. An
um 6zi. 316.87
i.~~rd l/Z

.ACC NR- AP6G21819 SOURCE CODE: UR/0413/66/000/012/0111/0111
TOR: Nabiullin, F. Kh.;_Lidorenkoy__j!,~,,_qt; Pen1kova, L. F.; Sladkov, M. S.;
Gertaik,Ye. M.; Buzova, Z. M.
ORG: None
TITLE: A method for producing spherical solar energy concentrators. Class 46,
No. 182962
SOURCE: Izobreteniya, promyshlennyye obraztsy, tovarnyye znaki, no. 12, 1966, ill
TOPIC TAGS: solar energy, epoxy plastic, geometric form
ABSTRACT: This Author's Certificate introduces: 1. A method for producing spherical
solar energy concentrators. This method consists of forming the solar energy concen-
trator elements from solidifying materials such as epoxy resins and plating the work-
ing surface with a mirror-like metallic coating. Production is simplified by placing
the solidifying materials between synthetic films clamped together by a frame on a
dead base. One of these films is metallized and the cavity between the base and the
film is compressed by air to give the proper shape to the concentrator. 2. A modifica
tion of this process in which the concentrator is reinforced by placing material such
as glass cloth or metallic rings along the edge of the concentrator between the films.
3. A modification of this process in which the metallized film is removed when neces-
sary after the concentrator base has been set.
~
ISUB CODE: 13, 1l/ SUBM DATE: O8Dec62
rd 1/1 UDC; 535,872.002.2;621.

ACC NRt AP7008488 S 0 UR-C- IE-05 0--D-* E-TIW620/611 06QO 02 10 0 Of,
AUTHOR: Lidorenko, N. S. (Corresponding member AN SSSR; Doctor of technical acienceal
Professor-r-
ORG: none
TITLE; Some problems of solar energy convertor
SOURCE! Elektrotekhnika, no. 2, 1967, 1-3
TOPIC TAGS: thermoelectric convertor,solar battery, "o a,- '-'jj to n^-4446Z~Q
jockz'_ tkd~ jz-Utt%_ jt*%&A&_K t- .
ABSTRACT: Several small grouln solar-energy converting stations have been designed
and tested in the USSR. Two automatic stations (about 1 kw, each) using photocells
are shown in Fig. 1. One station has 9 mirror solar energy concentrator formed by
a ribbed*surface which ensure a 2.5 times greater photo-cell illumination. The
second stationhwaparabolic concentrator which consists of plane mirror facets
providing an 8 to 10 times greater photocell illumination (the area of photocell
bank is about 2 m2). A third type, a thermionic converter,'with a parabolic concen-
trator (1 m2 for each 60.to 80 w) is shown in Fig. 2. Several types semiconductor
materials are presently, being.produced for thermal energy conversion. The first
ground thermal converter was tested in the USSR in 1955 and the first gace conveter
in 1961. These materials provide solar-to-electric energy conversion with an
efficiency of 12-15% at a 1000-0*C temperature drop. The thermal and thermionic
621.472.001.1
Card 1/2

ACC NRt' - AP7008488
converters are not so expensive as photocell converters lut their life Is "uch
shorter. Orig. art.6 has: 2 figures.
rwP1

ACC NR- A117005615 SOURCE CODE: UR/0413/67/000/002/U052/003
INVENTOR: Bclevtsev, A. T.; Dudkin, L. D.; Yerofeyev, R. S.; 4idqTq N. S,;
'Khanin, M. A.
10RG: none
TITL9: A method for manufacturing thermoelements. Class 21, No. 190448 [announced by.
the All-Union Scientific Research Institute of Current Sources (Vsesoyuznyy nauchno-
issledovatel'skiy institut istochnikovtoka)]
SOURCE: 12obreteniya, promyshlennyye obraztsy, tovarnyye znaki, no. 2, 1967, 52-53
TOPIC TAGS: thermocouple, temperature sensitive element
1ABSTRACT: A method of making thermocouples with a variable concentration of electric
)current carriers along the operating temperature gradient is introduced. To assure
both optimum variable concentration of the carriers and thermodynamic stability of
ithe elements, the amount of alloying impurities in the carrier concentration is
0
[determined by the specific solubility of the alloying impurities, thus assuring the
1desired relationship between the carrier concentration and temperature-i.e.,.
T3/4. [JR]
SUB CODE: 09/ SUBM DATE: 29Jul65
Card 1/1 - - - UDC: 621.362.1

ISKRZHITSKAYA, A.1.,; LIDOY, I.P.,; PETROVA, K.Y.
Propbylactic affect of bicillin in wound infections. Antibiotiki,
Moskva 9 no.2.33-36 Mar-Apr 56 (W-RA g.-3)
1. Kafedra m1k:robiologii (oav.-ohlen-korreBpondent AMN SSSR Prof.
Z.V. Yermollyeva) TSentrallnogo inBtituta usovershonstvovaniva
vrachey i Goopitallntqa khirurgLahookaya klinika (zar. prof. V.S.
Mayat) It Hookovokogo gosudaretvannogo meditainakogo institute,
imeni I.V. Stalina.
(WOUNDS AND'INJURIES, compl.
infect., prev. with benzathine penicillin G)
(INFECTIONS
wound infect., prev. with benzathine penicillin G)
(PENICILLIN, deriv.
benzathine penicillin G, prev. of wound infect.)

LIDOV, I,P.., dotsent; NESHKOV, T-V-, kand.meditainskikh nauk; STXPANSKIT, G.A.,
prof .
The Great Medical Incyclopeclia is a valuable aid f or the military
physician. Voen.-med.zhur. n0-7:83-90 Jl '59- (HIRL 12:11)
(MEDICINF,-DICTIONARIF,S)

ZAVALISM, N.I., prof,.,- LIDOV I P dots.; LITOVCHENKO, I.G.; MESHKOV,
V.V.J. dots.; M B SKIYp M.B., kand. med. nauk; ARTEMIYEVI
S.G.J. red.; BULIDYAYEV, N.A., tekbn. red.
(Organizational principles in providing medical care for troops]
Oanovy organizataii meditsinskogo obespecheniAa voisk. Moskva,
Medgiz, 1961. 219 P. (MIRA 15:2)
(RUSSIA-A[W-4SDICAL CARE)

-f--
LIDOV LP dotsent
I---- , I - , , I -,
Problem of terminology in military medicine. Voen,med.Zhur.
no.9.18-20 S 161. (MM 15:10)
(MEDICINE9 MILITARY-MMNOLOGY)

LIDOV.. I.F., prof.; RMCH, G.G.., kand. mad. nwak (Moskva)
I Improvement of the training of physicians. Zdrav. Roo* Feder*
8 no,,305-39 Kr'64 (KM 1724)

"Research on the category of trajectory in the restricted problem of three
bodle a . "
report submitted for 15th Intl Astronautical Cong, Warsaw, 7-12 Sep 64.

EW-N
--ACC-NR-- SOURCE GODE: Ult/9-612A6/()00/185/0064-/00()~
AN7002762
AUPHOR; Ligg&.-M. (Doctor of physicomathematical sciences)
ORG: , none
ILE: Thus changes the satel
Tr
lite orb'it
SOURCE: Pravda, 04Jul66, p. 4, col. 2-5
TOPIC TAGS: lunar satellite, satellite orbit / Luna-10 lunar satellite
ABSTRACT: The last radio contact was made with "Luna-1011"'on 30 May. If
only lunar attraction was involvedp and the diaEr-ibutf6a of mals's within
the moon was symetrical, the station would remain in its.orbit forovere.
llowovorj.ito inotion io affected by the as:mxiotrical distribution of
lunar rMIS3 and the attraction of the sun and earth. Solax~ attraction
.is 160 times less than that of the earth. 7no motion can be considered
as motion in an ellipse whoso parameters gradually change. It is diffi
cultila predict tho lifotimo of the satellite because the anomalies of
'the lunar gravity field aro-unknown and thia is a problem which can bo
solved on3,v bi oboorvationa of ovolution of the oaSollito orbit* Per-
Aurbations of the aun'and earth are known quite precisely* It could bo
assumed that the moon has a spherically symmatrical:*distribution of
mass or it could be postulated that the lunar grwrity field corroopond(I
-to a homogoneoua triaxial ellipdoid, (Tho paramotoro of sucli.& field
.aro known from observAtione ot lunar phyoioal libratione) Tho known
;orbital paramotera of tho eatollito Mako it.ponsiblo to copipute tho
47

ACC.NR: AN7002762
orbital evolution for either case, It may be that in the next 500 days
,the height of the pericehter of the orbit will increa3e to about 500 kmo:
.The semimajor axis of the orbit would remain virtually constant but the
.height of the apocenter would decrease by this samo*valuee Four years
after initial oribiting tho height of tho poricontor would bocomo looo
.than tho lunar radius and the satellite would fall to the surface.
During this time orbital inclination would have changed only 11 degrees.
During its lifetime the satellite would have turned in its place by about
.800. In the second variant the prediction is quite different. The max-,
iTmim height-of the pericenter is attained in 695 months (2p150 km)9
Then the satellite pericenter would decrease and the satellite would
-fall to the surface in 2o5 years. During this time the angular distance
iof the periconter from the node would decrease by approximately 1200 and
I Computations suggest that It -1011
,the node would turn by 1656o Luna will
continue in orbit for severa3 7ears and then fall to the lunar eurface*
!Continuing observations*. of -orbital evolut~aion- will giye.~ ~Mor~jreciee
lifetime a IMS; 37.o7103
SUB OWE: 22 SUBM DATE: none
Y.

USSR/Mathematics - Hydrodynamics
Card
Autbors I Lidov, Me Le
Title I Exact solutions of equations of one-dimensional unstabilized mov'ements
of a gas# taking into-account the Newtonian gravitational forces.
Periodical I Dokl. AN SSSR) 97, Ed. 3-, 409 - 410, July, 1954
Abstract t By using some assumptions, reduces the solution of a system of differen-
tial equationq ex
prealaing.one-dimensional-unstabilized movements-of a
ma-ss. of gas having weight and spherical shape, to the solution of a pro-
blem on such a gas, starting to move from rest in a vacuum. One reference,
Institution
Presented by L. I. Sedov, Academician,.May 10, 1954

USSE/Physics Shock waver. FD-2851
Card 1/1 Pub- 85-4/16
Author Lidov, M. L. (Moscow)
wow
Title Theory of nonsteady movement of a gas taking account of forces of
gravity
Periodi~_-al Prikl. mat. i mekh., 19, Sep-Oct 1955, 541-550
Abstract The author discusses solutions of gas equations for slight devi-
ationB from the self-model statement of the problem as given by
L. I. Sedov (Metody podobiya i razmernosti v mekhanike (Methods
of simi-larity and dimensions in mechanics], edition III, State
Tech.-Theo. Lit. Press, 1954). Four references: e.g. M. L.
Lidov, "Finite integral of equations of one-dimensional self-
model movements of a gas," DAN SSSR, 103, No 1; "Theory of line-
arized solutions around one-dimensional self-model motions of a
gas," DAN SSSR, 102, No 6; P. Carrus, P. Fox, F. Gaas, Z. Kopal,
"Propagation of shock waves in a stellar model with continuous
density distribution," The ABtropbysical Journal, 113, 1951,
496-519.
Institution
Submitted May,25, 1955

&idgir, On the theory of solutions linearized about
'Tre- =1mensional self-similar Walinns nj a gas. DAL F1W
(0-1 Akad. Nauk SSSR (N.S.) 102 (1955), 1089-1092.
[Russian)
in the general case of unsteady adiabatic motion of a
Peroeclyga5 ar coordinates. the
cit co~refcrred to spherical pol
Ve ponents, pressure and density can be written,
with an obvious notation, ia the form,
V s" 0, 0), etc.,
0
()=ab-1k+31/mf(-Jm)1k+3)--R(A, v, 0,
where and v=E11 are dime,~:ionless variable
parameters, V,, Ve, V4, P and R dimensionless functions.
It is assumed that for r=O the motion degenerates'
into a. self-similar motion with spherical symmetry so,
that [Pj,.*=P0(A), etc. The effect of a small disturbance;
to a self-similar motion i's then represented by considering
t%, the general motion when t, is small. The problem can be!
redticed to that of solving a system of 5 equations,i
'linear in derivatives with respect to ).,0,0 and with
coefficients depending on the basic exact solution.
Using dimensional arguments, integrals of this system,
are obtained in the following two cases. (1) When the

Symmetry. (2) When the dependent var'iables-can be
written in the separable form-
P(AI 0. 0) =P,(A)P,(O, 0). etc.
Complete details are not.given. The author states that
other cases can I-v worked out and that the work can W
extended to &-~,,ss sn~iall deviations from self-similar
motions with cyktidrical or plane symmetry. M. HoU.

ussR/ Mathematics
Card l/ Pub. 22 - 9/46
Authors i Lidov_j X* L* - - -
Title i The finite integral of equations of one-dimentional self arranging (auto-
modeling) adiabatic gas movements
Periodical t Dok, AN SSSR 103/1, 35-36, jul 1, 1955
Abstract A reduction is pr~sented_ofequations expressing a one-dimentional adiabatic
movement of an ideal gas to the equations of self arranging movement (defini-
tion of such movement is given). Then, using the expressions of self-
arranging movement-for velocity,-densiLy-, pressure and mss, the equations
are reduced to a system of ordinary differential equations a solution of
which leads to obtaining an integral which is good for any self-arranging
movement. One USM reference (1954).
Institution Moscow 3tnte University im. 11. V. Lomonosov
Presented by: Academician L. 1. Sedov, April 21, 1955

M% L. and KARPEMO,
A. G.
f1concerning the Temperature Regime in Earth Satellites," a paper presented
at the Eight Annual Congress of the International Astronautical Federation,,
6-12 Oct 1957, Barcelona.

AUTHORS: Karpenko, A.G.)and Lidov, M. L. 49-4-16/23
TITLE: On the temperature regime in an artificial Earth
satellite. (0 temperaturnom rezhime iskusstvennogo
sputnika zemli).
PERIODICAL: Izvestiya Akademii Nauk SSSR, Seriya Geofizicheskaya,
1957, No.4, Pp. 527-533 (USSR)
ABSTRACT: Papers published on the temperature regime in artificial
satellites are devoted either to evaluating the extreme
values of the temperature,which cannot be achieved in
reality or to the influences of the individual factors,
for instance, the molecular heat flow (Refs 1-3),
corpuscular radiation of the Sun (Ref.4), e;c. Such an
approach does not permit a sufficiently accurate
determination of the possible range of fluctuations of
the temperature of the satellite during its movement
along an orbit. The authors of this paper assume
infinite thermal conductivity of the body of the
satellite and also that the satellite has no definite
orientation whatever in space and these assumptions
enable disregarding the concrete design parameters of
the satellite. For certain circular orbits calculations
Card 1/3 ware made and graphs were plotted of the minimum and

49-4-16/23
On the temperature regime in an artificial Earth satellite.
Maximum temperature'reached by the body as a function
of the power of the'internal sources of,energyand i -ts
heat capacity for..a.oharacteristic.6-re"a i-~d`a
characteristic reflection coefficient of the surface,
In the calculations the energy from internal sources
from direct solar radiation and also from the Earth ?the
thermal radiation of the Earth and the reflection of the
Sun's radiation) were considered. The derived formula,
Eq.(19)tp.5311 is utilised for determining the tempera-
ture for two types of orbits, one circular in a lane
perpendicular to the line Earth-Sun (graph Fig.55 and
one with a circular orbit in a plane passing through the
line Earth-Sun. In both cases it is assumed that the
orbits are at distances of 200 and 100 km from the
surface of the Earth. By giving a satellite a definite
orientation the temperature conditions can be influenced
appreciably; the finite heat conductivity of the body
also brings about a change in the results. It can be
seen from the graphs that,in presence of small internal
sources of energy in the satellite, the temperaVre
Card 2/3 inside the satellite will vary between 0 and 10 C.

00 Vj fill. L.
AUTHOR: Lidov, M,L. 49-12-13/16
TITLE: Resistance of a don-orientated Body During its Movement
in a Rarified Gas (Soprotivleniye neomiyentirovannogo tela
pri dvizhenii v razrezhenaom gaze)
PERIODICAL: Isvestiya Akademii riauk SSSR, Seriya Geofizicheskaya,
1957, bo.12, pp. 1524 - 1528 (USSR).
ABSTRACT: A body moving in a free-molecular flow (particularly an
artificial satellite in the region of the upper atmosphere)
without its being specially orientated relative to its dir-
ection of movement, which is influenced by random distnrbancesi
will rotate with a variable angle of speed relative to the
centre of the-mass. The ideal non-orientated body introduced
in this rpaper permits calculating the average recistance of
such a body without calculating the resistances for individual
incidence angles. In the general formulation, accurate deter-
mination of the resistance coefficient of the sphere requires
calculation of the quadrature which depends on the parameter.
It is shown in this paper that it is possible to develop this
integral into series on the basis of the introduced parameter
and to limit the calculations to the first terms. Thus, the
Cardl/3,. E
_A'~.~q~aAcetcoefficient of the sphere is calculated on the basis
49-12-13/16
Resistance of a Aon-orientated Body During its Movement in a Rarified
Gas.
of a tabulated function- This
ofa simple formula by means er of investigations
can be.convenient for analysis for a numb re. If the
proposed to be carried out in the upper atmos~he
length of-the free travel of molecules of a current is larger
than the characteristic dimensionjs of the body, the ht.-at
exchange and the aero-dynaynic forces acting on the body can
be calculated on the basis of the kinetic gas theory. Die
regarding the distortion of the incident flow by teflected
molecules compared with the flow at infinityipermits consider-
able simpJification of the theory. The main difficulties
occurring in the given case are-caused by the character of the
reflection of the molecules and by the cumbersome calculations
required for complicated shapes. The assumption that.a Maxwell
distribution of the thermal movements of the molecules takes
place leads to the relations expressed by eq. (l ' 1525,
1 3 Calcu-
which are based on work by other authors Refs.?,
lation of the resulting aero-dynamic force due to ge reflected
molecules is reduced to calculating the normal pressure by
means of formulae (12) and (13)) p.1525- The full frontal
resistance of the non-orientated body can be calculated by
Card2/3 means of the eq. (17), P-1526- The resistance coefficient of

AUTHOR; Mdov, M. L. 33-4-9/19
TITLE: Aut~model motionslof a gas with spherical symmetry in
a field with a gravitating centre. (Avtomodel'nyye
dvizheniya gaza so sferichaskoy simmetrim v pole
gravitiruyushchegoteentra).
PFMODICAL: Astronomicheskiy Zhurnal, 1957, Vol. 34, No.4,pp.~Q 6 8
U29R3
ABSTRACT: In a previous paper'-(Ref.1) the present author gave a
solution of the problem of a central outburst in the
Roche model for'the adiabatic coefficients Y = 5/3 and
~ = 3/2. A special solution was found which was a
function of one independent variable (automodel solution).
In the present paper a more general formulation of the
automodel probleii is given for the non-stable motion of
a gas in the field of a gravitating centre using ideas
from dimensional analysis, Two integrals of the system
of ordinary equations for any value of the adiabatic
coefficient are given corresponding to the problem
considered in Ref. 1. For Y = 4/3 an exact solutionwas
obtained using a quadrature. The method was based on
the book by L. 1. Sedov (Ref. 2). Figures 19 21 3 show
the distribution of velocity density and pressare for
Card 1/2

LA
LIDOV, Ii,
Scouts of the universe. Rabotnitso 35 no.8:22-23 Ag '57. (KLRI 10:9)
1. HauchWy sotrudnik Komissit po moshplanotnym soobehahonlyam pri
Astronomicheskom soyste Akademit nauk ME.
(Artificial satellites)

Iasi
ns
.1-4
Z. IRM335:9 4
Up !lifaIlliq
r9l i I INJ f : 113
W.14
Is
Is
Set 8
sic 4- 913 9
0. JAVV4. 1 10'., j IC-21 di I
1113
jai 9

A
AUTHOR i Lidov, JI,L. (lionoov) 47-58-1-2/35
TITLZe Artifioial Zarth Satellites (Inakustvannyye sputniki zemli)
PERIODIGALs Fizika v Shkolep 1958, 11 it pp 6-21 (DSSR)
r
ABSTRICTs The goal in launching earth satellites is to obtain new
data on conditions in the upper layers of the atmosphere.
Until now our knowledge of the atmosphere in the higher layers
was based only on indirect observations. Such satellites are
of prime importance in studying the dispersion of cosmic rays
over the different parts of the earth. A table which calcu-
lates the "life-span" of a satellite rotating around the earth
at different heights, is given. Speciql devices in these
satellites will help to study the temperature variations in
space and to ascertain the ability of the earth's surface to
reflect various kindg of rays. As the final destruction of
artificial satellites is unavoidable at present, the study of
their orbit is useful to help scientists to develop a method
to brake their re-entry speed. A slow spiralling course would
suvs;aft serve the purpose and avoid the excessive friction which causes

LIDOT, H. L.
--a i -
I)etermining atmospheric density by observed deceleration of
the first artificial earth satellites. lsk.sputeZeme nool:
9-20 '58. (KIRA 12:2)
(Artificial satellites)
(Atmosphere, Upper-Rocket observations)

AUTHOR: Lidov SOV/20-120-6-16/59
TITLE: On Limit Solutions in the Vicinity of a Singular Point (0
predellnykh resheniyakh Tblizi osoboy tochki)
PERIODICAL: Doklady Akademii nauk SSSR, 1958, Vol 120, Nr 6,~ pp 1224
1227 (USSR)
ABSTRACT: In the paper under review the solution of non-linear equations
in the vicinity of a singular point is investigated at a test
problem. Information concerning the construction of the.limit
solutions in the general case is presented. The author.pro-
ceeds from the equations.of-the one-dimansional not yet steady
adiabatic motions of an ideal gas (Rof 1). non the exponent
of the adiabatia curve is 7j the automodel-like problem of a
heavy punotiform explosion in a medium of constant, density
possesses a simple solution W1110h io SiTen. When the complete,
non-,linear system of partial differential.equations is line-
ariied in the vicinity of this solution it is possible to
solve the not automode-l-like problem ofa, heavy punctiforn
explosion in a medium with a definite initial density distri-
Card 1/,;~ bution. A start for the solution of this s"tem of dif-

On Limit Solutions in the Vicinity of a Singular Point
SOV/20-120-6-16/59
ferential equations is written down. As a result of the line-
arization presented a system of ordinary equations with con-
stant coefficients is obtained. Three special cases are in-
vestigated. A treatment similar to that employed hitherto
leads -to a method of the construction of the limit solutions
in the more general case of spatial.parturbations of a one-
dimensional automodel-like motion in order to obtain the
solutions in the vicinity of the center. In this case the author
as a practical foothold considers one-dimensional spherical~
symmetric automodel-like problems. The dimensionless solution
of the axially symmetric equations of unsteady adiabatic
motions of an ideal gas are set up in the form of series. The
determination of the coefficients is outlined in short. The
equations and boundaxy conditions in the vicinity of the center
can be simplified also in the case of perturbations in the
vicinity of one-dimensional automodel-"Like motions with a plane
or an axial-symmetry. This can also be done in the general
case of spatial perturbations. There are 2 references,
which are Soviet.
Card 2/k
; ~~

26832
S/560/61/000/008/001/010
1 .2 zoo E032/E314
AUTHOR: Lidov, M.L.
TITLE.- Evolution of Artificial-satellite Orbits Under the
Action of Gravitational Perturbations Due to
External Bodies
PERIODICAL: Akademiya nauk SSSR, Iskusstvennyye sputniki zemli,
19610 N0.8, PP-5-45
TEXTt Published'papers on the evolution of artificial-satellite
orbits'have been concerned'with the detailed'analysiar
6f the effect of non-central contributions to the Earth's
gravitational field on the satellite orbit, and-the braking
effect of the Earth's atmosphere. Some-workers have-also
consi&ered-finer effects associated with the rotation of the-
Earth's atmosphere-. Changes in the latus rectum due to the-
giravitational attraction by the Moon and'the Sun were only
estimated approximately. These estimates showed that for low..;
lying orbits the latter effects-could not be measured*with -- X
existing apparatus. However, d6tailed-analysix of the orbit
of Vanguard-I showed (Ref.1 - P. Musen et al, Science, 131,
Card*1/14

26812
S/560/61/000/008/001/010
Evolution of R032/E314
935 1960) that the observed evolution of the latus rectum could
not be explained without taking into account the attraction
of the Earth and the Sun, and even the light pressure-.
The first case, where the gravitational attraction of the Moon
and the Sun had a great effect on the satellite orbit, was that
of the Soviet Automatic Interplanetary Station which was
launched on October 4, 1959. Lunar and solar gravitational
6ffects are equally important for satellites of the type
of "txplorer YXII. In studying the evolution of
artIfIcial-satellite orbits, it is, as a rule, necessary to
investigate a relatively wide (in the general case, five-
dimensional) region of the possible values of the parameters.
The use of exact solutions of systems of differential
equations in this connection, even when these solutions are
obtained with the aid of fast computers, would require a very
6onsiderabl*e amount of time and labour. It is therefore useful
to develop-approximate analytical methods. F.T.Geyling
(Ref.5 - J.'Prankl. Inst., 269, 375, 196o) has reported this
type of work. The aim of the present work was to derive the
Card*2/14

26812
S/560/61/000/008/ool/olo
Evolution of ... E032/E314
simplest possible formulae for the approximate investigation
of the evolution of a sufficiently wide class of satellite
orbits. The basic assumption employed is that the ratio of
the height of the apocentre to the distance between the
perturbing body and the central body around which the satellite
is orbiting is sufficiently small* This assumption limits the
class of orbits which can be investigated by this method.
However, for an Earth-satellite for which the height of the
apogee is 50 000 km, the secular variations in the orbit
elements can be calculated to within 1-3%. Another assumption
which is used in the derivation of formulae for the changes In
the orbit elements is that these changes are small. The overall
problem is formulated as follows. Suppose that at a certain
instant of time the following osculating elements of the orbit
of a satellIteg moving in the field of a central point with
a constant gravitational potential I& , are given:
p - parameter of the osculating ellipse; e - its
eccentricity; w - angular distance of the pericentre from the
node; I - inclination of the orbit; true anomaly;
Card 3/14

26812
s/56061/ooo/oWool/olo
Evolution of ... E032/E314
u = w +,I, and 11 - longitude of the ascending node.
The angles i, w, 11 and u are measured relative to the plane
OXY , which moves together with the central body. The XYZ frame
does not rotate in absolute space. The motion of the satellite
in the field of the central point is subject to perturbations
due to gravitating points characterised by the gravitational
constants Pk(k = 1, 2, ...). The positions of these points
relative to the central body are given by the radii vectoAs
rk(t) - The effect of the mass of the satellite on the
central and perturbing bodles Is neglected and the perturbing
points-are aesumed-to move-over elliptical orbits around the
central point. In that case, r (t) is determined by the
% k
elements pi, ek9 Wk9 Xzkl uk and, 'k It is also assumed
that the satellite .1atus rectum and the perturbations are such
that the osculating orbit does not depart during a single
revolution of the satellite from an elliptical orbit with fixed
Card 4/14

26812
S/56o/61/000/008/001/010
Evolution of .... E032/E3.14
parameters corresponding to the values of the osculating
elements at% May, the pericentre. The approximate formulae
describing the evolution of the satellite's orbit are
derived from the following equations of motion ,
(D.Ye. Okhotaimakiy, T.M. Eneyev,.G.P. Taratynova.-
Ref. 6 - UFN, 63, No. la, 33, 1957), in which the independent
variable is the true anomaly
dp 2rt T,
dF
de rty S sin 0 4 (1 + -L) T t-o,;,D +T],
T, P P
d,
t 3 Cos 0 + (1 L) 7'An 0 - e-LW H,g i Hin u),
d-6 pe P P P
dg Ply W sin is
diF itp i-Ini
dl tW Cos I,
Card 5/14

s/56o/61/ooo/oo8/ooi/o1o
Evolution of E032/E314
where
+.L S Cos _'L"(t + L r,i.0
P)
(2)
In these expressions, S, T, W are tfie components of the
perturbing acceleration along the radius vector, the perpen-
dicularto thisradiusvector whichlies in the plane of the
osculatingellipse and the perpendicular to the pl'ane of the
osculating ellipse, respectively. The perturbing acceleration
F(k) experienced-by a satellite at a distance r from the
"Eentral body, which is due to the k-th gravitating point, is
given by:
(k) Ek E Ekl.
Ilk( (3)
j!:k rk
where rk is the distance of the gravitating point from the
Card 6/14
J

268,
S/56o/Wooo/oWooi/olo
Evolution of .... E032/B314
and on the s,econdapproximation
S(k) - 15 Ilk r2
COO (0 - 0,
-T '5 Cos
.2k '.'k
'
15 Pk PS t3 C082 04) oil, (D
1-k
rk'
~V(k) 15 Rk r%
"k [t' COS2
In thbae +
expressions, 1 2 is the true
anomaly of the projection of the vector Ek onto the plane
of the satellites orbit and sin-ky, cos-J
r. is then expressed in the form r k Pk~~k where Pk
is the characteristic distance to the perturbing body and
k is Lao given dimensionless positive function of time.
Card 8/14

26612
S/56o/6i/ooo/oo8/ooi/oio
Evolution of .... E032/E314
When the orbit of the perturbing body is an ellipse, then
Pk is the latus rectum and + ek Cos Using the
relation r = pIZ3 , where /-A 1 + e cosY , the expression
for S, T and W can be rewritten in the form:
(8)
Menonbayn conTHomenHe.r rAO e C080, momno nmpnme-
man Ann 8, T, W nepenncaTL 8 BHAe
,S(k)
I coO 0 2P, cos 0 sin 0 + P, sin' 0
3 1P 3 1
Pk
T(Ik)=-3t-k.L (P,--:p2)cos0sinO+P,(ainl.%-cOS24)
A
PP, Pk
'k
W,k)=3L.L PIsCOSO+P48ia.& A
A Pk
Card 9/14

268!2
Evolution of .... S/560/61/ooo/oo8/001/010
E032/E314
CYR) M ILk IA
2,p [Ticos"O-F3T:Icos'OsinO+3,rcosi)sin2O+I
k 1,2
-l-,r2sin3,o--!,Icoso-~-ce2silliD
5 5
(k) 15' Pk P2
T
2 - 2TG) CC).
2 42 Pk2 P T.-, COS' ' 0 + (Ti 2 0 sin 0
+ (2ya-y2) Cos 0 sin2 iD+T. --in-' 0- sin 0 4 -L Cx-2 Cos 011
F;101
5
W2(k) =15 Rk
wh er e 2 -,2k 1,2 IT4 coq2 0 + 2,r, cos 0 sin 0 + TI, sin2 0
At -
(9)
Card 10/14

Evolution of
3Aech 6maif nneAwtm 060311OW11161:
at 91A'k, a2 = t2A'k,
=L- UAI P2 = E'2A'k

04 EAAL
0, ~ Elt.1M.
k
Tt VAI 'r2 = uA4k ,
4
-r4 BTE.,Ak
t2 ,A4,
k
-r-.
2681-2
S/560/6l/Ooo/oo8/ooi/oio
E032/E314
OC3 ~-LA'kl
P3 = EIE2Mk,
(10)
P, = A"k,
= ~2192At,
-r.
k#
X
It follows from Eqs. (2) and (6) that ihe maximum value of y-1
3.LS of the order of magnitude 6 f (Ii Ic /14(a/rk )3. / a , in the case of
small eccentricities and (pj,/V)(a/ (1-e) in the case of
I rk)
eccentricities approaching unity (a is the semimajor axis).
In many cases, ono can assume that y = I and this approximation
Is, In fact, used in the present paper. The-next assumption
Card 11/14

5/56061/ooo/oWooi/m
Evolution of .... F,032/E311,
is that in determining the secular variation in the elements
the various component perturbations can be evaluated separately
and the total erXect can be obtained as a simple sum,
eog. 6 p =7-A- pit etc. Finally, it is assumed that the
quantities a Pi and yi can be written down in the form
of the series
+
dt
POI + (L")'At -" - IC2-1), (At)2 + ....
di 2 di2
C= -r; + (Ly) *At + -L (dT')'(Ai)2 +
T
I di 2 -,I-t f
and it is sufficient to retain only two terms in each of these
expansions (A t = t - t4 I where t+ is a certain fixed instant
Card 12/14

2681 ~
S/560/61/000/00/ooi/olo
Evolution of * ... E032/F-314
of time). The remainder of the paper- is concerned withs,
a) derivation of formulae for the variation in the orbit
elements per orbital revollation of' the satellite!,
b) calculation of the paLrameters a.,, Pjj yi and their
I
derivatives in the caae where th,~; perhirbing body moves in
an ellipse;
C) derivation of the formulae for the variation in the orbit
elements for a nil ber of orbital revolutions of the satellite;
d) analysis of the equations for the secular variations In
the orbit elements~
e) estimate of osGillations in ths height of the pericent-re
of the satellite's orbit!:
f) method of caloulation of the evolution of the artificial
satellite7s orbit using the approximate formulae-,
g) comparison with results obtained by numerical integration
on the differential equationz.
It is shown that in the caae of orbIts of the type followed by
Explorer VI, for which the height of the perigee is of the
Cax'd 13/14

S/560/61/000/008/001/010
Evolution of .... E032/E311k
order of the Earth's radius and the hei9t of the apogee Is of
the order of 50 000 - 70 000 km, the approximate formulae give
the correct results to within less than 5%. It is conclud6d
that the approximate farmulai4 de-Y-61.op6d in the present paper
can be used in the analysis of a sufficiently wide class of
satellite orbits and, in particular, thoee whIch are followed
in cosmic flights. AcIsnowledgments arb -,~rpressed to
D. Ye. Okbotsimakiy- for a number of suggestlons
There are 9 flguras~ I table and 10 raferanc.t_a~ 6 Soviet and
4 non-Soviet. The three En.glish-languagte. references quoted
are: Ref. 1 - P. Musen et al - Scien,-,e, 131. 935, 196o;
Ref. 4: C.P. Sonett, E.I. Smith, D.K. Judge, P.J. Coleman -
Phys. Rev. Lett., 4, 161_19fo- Ref. 3 - F.T. GeylIng -
J. Frankl. Inst., 269, 3-7,,:, tg6c.
SUBMITTED: December 7, 1960
Card 14/14

"On a method of investigating orbits in a restricted three-body problem".
report presented at the 2nd All-Union Congress on Theoretical and Applied
Mechanics, Moscow, 29 Jan 5 Feb 64.

Kosmicheskive issiedovaplya. z no.
77tt!-!f;ej, -~-41-f-rf?ft trqipcf-nr-,,, fiiLTht traiectorv,
Fnf,'VeV (j',OSMj4Cn.

N Nli: A P 4 0,16 7 7 5
r,~n f-hf. ~,aqiz nf th.-z~- 'AAql-lmlnlc3rl f;

LiGov, M. L. Okhotsimskiy. 0 Y(I
A'rj 1'.7 -1
;i*R(-'i,: Kosmicheskiye issledovaniya., v. 2, no 6, INN, 843-652
eciestial rnechanic~s, rnonn thr" li,Ov !)rohlom. spacecraft tra)ectory,
.9~1 a~,f-,cr;ift orbit
~71, A C T: The authors propose a method for investigating a class of tra)ectories for
from the varth In Lhe rnwin in whi-h ni rather aPproach to the
OLII e I i6 ciass of trae<
6')
Since the pa r"
t lie f, a r t-h 'v,, i
-,-~irescatation oi Me Derav
-GaL 'IV
F. I ithdrawal o, th,2 s-a( r, m t, r,- W'. e
',rajectory close to a conical section eimer to -n e~'ipse -i T
a' t e 'imzis of ih~s sphere
a2uence or to a hyperbolic cur%e emerging beyo," ~h I
m. .:-C-6e of LhLis article is a study of the para-mieters of tr-iiecwrliea in :iiis rl'--Ctinn

21~-04-6
.5
ACCESSION NR: AP5000166
.ce -f th(-. ~reocenztric parameters of orbits
tne -lutflors Consider the
7-- 0 1S
near trajectories arc ~L
on
Ln ma-King
M -kd s aii.' F
ations for LWs study." C~rjg art ziab.
ASSOCIA-11ON: aone
i~,V: ED: IOAug64 ESCL: 00 SUB CODE: SV, AA
SGV: 000 07'HER: 000
2, 2

-1 45-2-5--r--66 i"~il)/EM(k )-2/-FCC
AP6020934 SOURCE CODE: UR/0029/66/000/006/0008/0011
AUTHOR: lw2v.,- M. L (Doctor of Physical and Mathematical Sciences);
Lebedinskiy, A. I., _(M-etor of Physical and Mathematical Sciences, Professor);
Vernov, S. N., (Corresponding Member of the Academy of Sciences SSSR)
ORG: none
TITLE: The battle for the Moon continues
SOU+11CE: Tekhnika-molodezhi, no. 6, 1966, 8-11
TOPIC-TAGS: moon, space, lunarsurface, lunarradiation, lunarlanding
/Geigercounter, Luna9, LunalO
ABSTRACT: The interviewer reviews briefly the history of lunar research,
presents a table of chronology and facts and repeats questions and answers.
Dr. M. L. Lidov stated that one of the problents solved by Luna 9 and Luna 10
was that of landing at the most favorable time, 4.. e., lunar daybreak. A n_o___th*er_
problem was the selection of the most "economic2l" trajectory along which to Ben'd
the heaviest apparatus. He stressed the importance of human initiative in the
Card -11~

1. LIDOV, V. P.
2. U3SR (600)
4. Geology and Geography
Essays on the Physical GeograplW of Gork:Ly District,, S. S. Stankov.
(Third revised edition, Gork-ly Regional Press, 1951). Reviewed by
V. P. Lidov, Sov, Wga, No. 7, 1952*
9. IWReport U-3081, 16 Jan 1953, Unclassified,

PA 196T69
"1~rom Faperience Gained in Conprehensive Geogra-
Phical Investigations," V. P. Lidov
":Ez ik Itauk, Ser Geog" No 2, pp 71-80
-Describes qxPerience of Moscow State U and Geog
Inst.,.Acad Sci USSRj during investigation'of' Cen
Chernozem Belt,ln corme6tion with Stalin's plan
to transform nature. These results cause the
author to appraise unfavorably the article by A.
M. Snd=ov "FUndamentals.of Geogmphical Science"
("Voprosy Filosofii" No 2,--1950).
1961%9

-GVODETSKIY,-N#-A-o -LIDOVP V.P.
Physical Geography
Discussion of the report of N.V. Dumitrashko,, L.G*. Kamanin, and Yu. A. Heshcheryakov,
"State and problems of contemporary geomorphology." N.A. Gvozdetskiy,, V.P. Lidov.
Izv. AN SSSR Ser. geog. No. 1, 1952
Month],y List of Russian Accessions, Librar7 of C-ngress, April, 1952 LWCL

V. -F-*- -
USSR/Cleophysics Europeau UB8H may 52
"The.Future of the Central Chernozem Region,"
V. P. Lidov
loptirods" Vol 41, No 5., PP 38-48
Describes Stalin plan for transformation of nature
as it applies.to the general territory of European
USSR, particularly the central chernazem zone, in-
c1fiding Tamboysk, Voronezh,--Kursk, and Orlov ob-
lasts. Stresses the problems of erosion and
scoured nature of the land, vbLich once was covered
by glaciers.
230T60

5
I- MDOVO V-.- P.; NIKOLAMNSKAYA'YE, m. - -- - - - - - - -
flaps
Improtance of spc6ialized maps for the geographer in solving the tasks of transforming
nature, Izv. Vses. geog. obshch., 84, no. 4, 1952.
Mont List of Russian Accessions, Library of Congress, October _1952. UNCLASSIFIM'.

Pab 4
clam 7-
Authors- I-Lidove-, Dik. N Ye'l Nikolaevskiy,, Ye.M.1 Setunskaya, L. Ye.1
andl~eleVaya, N. V:
Title ItClas sification of recent linear forms of erosion
Periodical Izv. AN SSSH. Set. 9009- 3, 91-99, May ;un 1954
Abstract I A-study iss made of Ahe -work- of classifying forms.of erosion along the
following-basic lines-, establishing qualitative differences of the diff-
erent-types of forms depending on the intensity of the erosion processes,
distinguishing between the types of forms in accordance with the stage
of development in evolutionary sequence and showing the nature of the
ut-eraoing-,, -irocesues-,on-the-bi-Iges-and-&Iope-a - of-t he-f orms,-Fiv a --MSR-
ubmitted;-

LIDOV, V.P.
, I , "Oefteffmom
Geomorphological, research for the needs of agriculture* Vop,gecg,
36:30-39 154* (KLU 8:4)
(Phys;cal geography)

LIDOV, V.P.- DIK, N.Te.; NIKOLAYEVSKAYA, Ye.K.; KENELEVA, N.V.
Still more about boundaries of geographical regions. Izv.Vses.
geog.ob-va 86 no.1:5?-66 Ja-F 154. (MLRA 7s2)
(Geography)

LIDOV, V.P.
Principles of diTision into physical geographical districts.
Izv.Veeo.geog.ob-va 86 no.2:169-177 Xr-Ap 154. (MLRA 7:6)
(Physical geography)

-USS111 oil Science Genesis and GcoL;raphy of Soils. J-2
.'s
Abs Jour : Ref Zhur - Biol., No 3, 1958, 1o464
Author : Lidov, V.P., Didurenko, ILF.
Inst :
Title Some Remarks on the Classification of Washed Oat Soils.
Orig Pub Pochvovedeniye, 1955, 140 11, 80-85
'tbstrac' The soil erosion indices used in the classifications of
A.S. Kozmenko, (1948) and S.V. Naumva (1955) must be
handled with extreme care under cer-cain zonal conditions
and with certain types of relief. It is recommended ~;h-z
the erosion in small channels and /razmoiny/ be taken
into consideration end that areas with broken up microre-
lief be distinguished from those where the microrelief
has been smoothed out. A classification of eroded soils
must contain a description of the angles of surface inclii-
ne as well as indices of the length of the slopes. For
successful develonment of a unified classification of
Card 1/2

jJPSR/Soil Science - Genesis and Geography of Soils. J-2
Abs Jour : Ref Zhur - Biol., No 3, 1958, io464
eroded soils, soil scientists, geomorphologists, and
hydrologists must conduct research together toi,-.xd uni-
fied objectives. This is as imortant as Mced observa-
tions.
Card 2/2

LXDGV, V.P., UMSZLU. L.Ye., MDOWA, N.V.
Q=titative studies of micro-relief assoclated with soil erosion.
Izv.Vses.g9og.ob-v& 87 no.6:542-546 I-D '55. OM 9-3)
(Brosion)

LIDOV. V.P.; SETUNMYA, L.Ye.
~Uft *
Cartographic research method
tional physical geographical
and problems of division into frac-
regions. Vop.geog.,no.39:70-79 '56.
(KM 9.11)
(Physical geography) (Cartography)

J
137-1958-3-4882
Translation from: Referativnyy zhurnal, Metallurgiya, 1958, Nr 3, p 61 (USSR)
AUTHORS; Lidoy, V. P., Blinova, V.A.
TITLE: Experience in Smelting Lead-copper Matte With Sodium Sulfide
(Opyt plavki svintsovo-mednogo shteyna s sernistym natriyem)
PERIODICAL: Sb. nauchn. tr. Gos. n.-i. in-t tsvetn. met., 1957, Nr 13,
pp 232-234
ABSTRACT: The shaft smelting of Pb-Cu matte was carried out under
industrial conditions. The matte was composed of 19.2 percent
Pb and 13.4 percent of Cu, with an addition of converter slag
(composed of 2.4 percent Pb, 1.3 percent Cu, 14 percent ZnO,
', 10.61 percent CaO, and
36.8 percent FeO, 28.8 percent SiO?
6.54 percent A1203), some industrial sodium sulfide (approxi-
mately 70 percent Na2S) , and some Fe- scrap; the charge
ingredients, namely: the matte, the converter slag, the sodium
sulfide, and the Fe scrap, constituted, respectively, 57 percent,
35.3 percent, 6.Z percent, and 1.5 percent of the charge. In com-
parison with the smelting of an analogous charge, but without the
addition of Na'ZS, the weight relationship Cu:Pb in the matte ob-
Card 1/2 tained increased from 1.9 - 2.6 to 3.8 (5.4 percent of Pb instead

,-LIDOV. V.P.; NIKOLATEVSKAYA. Ye.M.; SABO. Ye.D.
Practical plan for studying erosion factors and predicting the
occurrence of erosion* Isv*Tsesogeogoob-ya 89 no*1:43-32 AL-7
'570' (MLRA 10:3)
(Brosion)

Ya. Sh.
2ITILE: Conference on Bew Methods of Making, lead (Soves'--chaniye
po no-ryrq metodam, polucbeniya svintsa)
'IRIODICAL: Tsvetnyye Iletally, 19';)8, 1,Tr 9, pp '/2 - r/5 (USSR)
*- P U
.r.,STRACT: A conference on me'liods of lead orodljction froLi
concentrates was 1held ;311- tho Gints~eimet on Juac 22-25,
1958. Since tfe last i?.eetim~ in 1953, over 20 flowsheets
and variants have been testca by v~, 'rious -,.;orks and
organisations and the purpose of the present meeting was
to evaluate this work. Pre-prints of the following
reDor+-s h,-d been circulated: "On Electric SrieltinL-,- of
Lead Raw MaterialL' by A.P. S,,,chev, 'V.A. 1,,,-ik1-1eyev, D.A.
Sushchinskiy of vvIItsvetumet, A.V. Yulcov 3f Kavtaz-ipro-
tsvetrnet; "On Precipitation and Reaction Sraelting of
Lead Concentraoes" by V.P. Lidov, L.A. Blinova, MI.P.
Smirnov, L.A. Kudryashj-va -of Gintsvetmet, I-ff-Pd1yyyanyy-
et al. of the Institut metallurgii'. i obogashcheniya
AN KazSSR (Institute of Metal-j-urgy and Beneficiation of
of the Ac.Sc. KazSSR); "On Hydromeil-allurgical Treatment"
by A.n. Vol'skiy, R.A. Arracheva, A.M. YeGorov, P.S.T-itov,
le.M. Losku-tov and V.S. Lov-cTiikov of Min7E'~-vctnetzoloto
and A.K. Pomosov, A.I. Levin et al. of the Ural'skiy

uonfcrence on. vew Methods of T;Jakinr- Lead
politekhnichesk-4y institut (UrIals PolytecL--nIc I~,ztitutue);
on the "Electrolytic Production of Load bZ7 Eccj,rolybes
of li'used Salts" ty I.G. Grulld1n) A.V.
v.P. Barinova and Y.K. Ruppul' of G_'.--.)tsvetmc-111- and Yu.K.
DelimarGkiy, I.D. Panchenko, Ye.B. Gitmaia and. A.A.Kol,3tiy
of IOVKh Ac.Sc. Ukrainian SSR.*,O' The conf~2renlce was o-pened
by D.M. Yukhtanov, deputy director of Gintsvett-.,.et, -,;ho
discussed recent progress and noted that pred 4
U ictions
that the lead industry v-,rould develop in the dilrection of
the hydrometallurCical treatment of flotation concentr7tes
had not been fulfilled; he said that the -most hichtly
developed of the new methods wore electuic sii-.,eltini-.- end
electrolytis of fused raterial and thatcpyro--etallur.-ly
-he dis-
would retain its importance for a lon:~- ime. I n LI
cussion that follo,,-.-ed, D.Y. Chizil-ii'lzov corrt3c-rji)din,-:
member of t'lle Ac.Sc. USSR, systermatized and rrvie-,ed all
known procesces. P.A. Pozdniliov and A.A. Vlasova of LTFA.L7
described met-jl.ods of treatirtent develor-,ed tI:CrC; ul.; U
high effectiveness of .-;hicl, was dOubted by v.A.M-rchevelriy
d 5 of Gi-orotsvetriiet and s.I. Sobol' of Gintsvet.,,-n~5.

--e in 1jew Methods of Lead SOV/136-56-9-16/21
A.M. Zykov of the Leninr-rrad Polytechnic Institute criti-
cised the reports presented as being- insufficic-ritly
analytical. G.P. Vyatlev of the Ukrtsink Works recomnended
t-he adoption of electric instead of shaft smelting of
secondarj lead materials at the works. A.n. Vollskiy,
Corresponding Member of the Ac.Sc. of the lintsvetmetzoloto
described work he had directed there on sulphide oxidation
and recommend3d. more atteation to safety aspects.
v.!!*. Fedorov of the GnTK USSR drew attention to the
comparati-e lack of work in the Soviet lead industry on
new methods, but opposed the proposal by Gintsvetmet to
build a new, large electric furnace at the Leninogorsk
Works. P.I. Kravchenko of the Blektrotsink Works deplored
the incompleteness of all the work reported at the
conference. A.M. Lomov of Kavkazgiprotsvetmet considered
the adoption of electric smelting of lead concentrates
and I.D. Panchenko of IOIUM of the Ac-Sc. Ukrainian BSR
with electrolysis of fused salts. F.M. Loskutov,
Professor, Doctor of Technical Sciences of Mintsvetmetzoloto
reminded the conference that electric smelting is not
applicable to all materials and disagreed with Kostin's
suggestion that all Soviet works should be converted to

Conference on New Methods of M-aking Lead SOV/136-58-9-16/21
this practice; he also spoke against alkali treatment
of lead-containing materials - a view opposed by G.G.
Zapevalov of the Irkutskiy Eorno-metallurgicheskiy institut
(Irkutsk Mining-metallurgical Institute) who also stressed
the'need for economic evaluation. -:M.A.Chernyak of
Giprotsvetmet doubted whether electric smelting could
revolutionise the lead industry and urged more research
on the alkali process and sintering. I.V. Paramonov of
the Gosplan of the KazSSR criticised the research work
reported but D.N. Klushin of Gintsvetmet said that this
work had gone a long way to realise the aims set out at
the previous conference thouGh much effort had been wasted.
Mang speakers deplored the-lack of central direction of
rP--P*rnh,work. After putt'ing on record their views on the
proposed methodE, the conference decided that effort should
be concentrated on the study and development of
a) electric smelting of primary lead raw materials without
added fluxes and electric sreltin(~ of secondary materials;
b) electrolysis of lead concentro-tes in fu2;ed electrolytes
(for the rich materials of tho "Elektrotsink" and Sikhali
Works); c) electrolytic refininG of lead in aqueous

AUTHOR: Lidovj V.P, S07112-90-6-4123
TITLE: roblems of Physical Geography in the Next Years (0 za-
dachakh fizicheskoy geografii v blizhayshiye frody)
PERIODICAL: Izvestiya vsesoyuznogo geograficheskogo obshchestva, 1956,
Vol 90, Nr 6, PP 531 - 533 (USSR)
ABSTRACT% The author refers to the article of I.P. Gerasimov "Thermal
and Aquatic Conditions of the Earthis Surface, its Role in
the Dynamics of Natural Processes, Geographical Diversities,
and Methods of Transformation for Practical Purposes" (iz-
vestiya AS USSR, Geographical Series, Nr 4, 1956), which
was written in conjunction with several authors and dealt
with the fundamental problems of Soviet physical geography
for the coming years. By way of discussion, the author of
the present article expresses his views on the important
problems raised in the article which, in his opinion, is
a onesided outlined He quotes a number of questions on
which he agrees with the authors as, e.g., on the importance
of studying the thermal and aquatic conditions of the Earth's
surface, that only the first steps have been taken to ex-
Card 1/3 plain the general geographical laws, that it is necessary

On Problems of Physical Geography in the Next Years
SOV112-90-6-4123
to expand and intensify scientific-theoretical research, to
organize the special experimental work on a broader basis,
to elaborate the observations made by the hydrometeoroloe-
cal stations, etc. But, he P_ske pwho will take care
of these matters, since according to the plan neither the
soil scientists may be engaged in problems of physical
geography nor the physico-geographers take up the study of
geophysical problems, Criticizing I.P. Gerasimov's asser-
tion that one of the most.important means of a rapid rise
in agriculture, is a rational distribution of agricultural
production with due regard to the natural (thermal and
aquatic) resources of the country, - the author states that
because of methodologically wrong ositions, Gerasimov comes
to the false conclusion that a thorough study of the ther-
mal and aquatic conditions of the Earth's.surface is the
most important theoretical problem of physical geography
at the present stage of its development, if one is to
agree with this contention then what is the most important
problem left to the climatologists and hydrologists? In
Card 2/3 his further considerations the author indicates the working-

On Problems of Physical Geography in the Next Years
SOV/12-90-6-4/23
out of scientific foundations for the division into districts
as the most important theoretical problem of physical geo-
graphy. Another important problem is the composition of
geographical monographies on the republics and districts
of the USSR. In reviewing the article of Gerasimov, the
author finds that the problems of physical geography for
the near future have been greatly narrowed on the one side,
while on the other they have been much too generalized.
At the end he states that the country now requires as ne-
ver before good, complex geographical studies and thorough-
ly performed work on the physico-geographical zoning.
Card 3/3

LIDOV, V.P.; SMINSKAYA. L.Yn.
Results Otalned from investigating erosion processes by apply-
ing the quantitative cartbographic method on the banis of
invontigations in the Volga Upland. Trudy Inst.lana 44:5-34
'59. NUM 12-.9)
(Erosion)

w
LIDW, V.P. -, DIK, N.Ye.; NIKOLAYXVSKAYA, Ye.14.; KH16LEVA, N.V.
w
Bo ttom gullies and their development; based on studies in
key areas of the right banics of the Don. Trudy Inst.leea 44:
101-137 159. (Don Valley-Srosion) (MIRA 1229)
1

LIDOV, V. P.
Some 6haracteriatice of erosion processes In ravine systems and
phasic development of the Interior morphology of ravines. Test.
Moaks, uns Sere 6: Mole, pochv. 13 no.4:61-67 JI 16o.
-%RA 13:10)
lo Wedre, fisiki I mollorataii pochv Moskovskogo un4versitet,a.
(Arosion)

,. LIDOV V.P. - ILMZRDINA, M.V.; PITREM, I.A.
Mfect of light on the development of steppe vegetation in
forest stands under conditions -prevailing in West Xazakbotan
Province* Vopegeog .*. noo48t223-241 160. (MIRA 1397)
(West Kazakhstan Province-Yorest ecology)
(Plants, Iffect of light on)

GAYELI, A.G.; LID0V, V.P.
Problem in the study of soil erogion and its control. Hauch.
dokl. vys. shkoly; biol. nauk4,no-4t178-185 161. (MIRA .14:.U)
1. Rekomendovana kafedroy fiziki i melioratsii pochv Moskovskogo
gosudarstvennogo universitata im. M.V,Lomonosova.
(SOIL CONSERVATION)

KOSOV, B. F.; LIDOV, V. P.
First intercollegiate conference on soil erosion and measures
for its control. Nauch. dokl. vys. shkoly; biol. nauki no.3:210
162, (MIRA 15:7)
(EROSION-CONGRESSES)

AFANAS I YEVAp T. V.; _LIDOVZ_ V- F.
Using aerial photographic materials In the investigation of soil
erosion by water. Nauch. dokl. vys. shkoly; biol. nauki no.3:
194-198 162. (MIRA, 15:7)
1. Rekomendovana kafedroy geografti pochv Moskovskogo gosudarst-
vennogo universiteta im. M. V. Lomonosova.
(PHOTOGRAPHY, AERIAL) (EROSION)

LIDOV,.-,V_.P.,- ORLOVA, V.K.; TYURDENLVA, S.A..
Dust storms in Stavropol Territor7 and measures for controlling
them. Goeg. i khoz. no.12:29-39 163. ' I(MIRA 16:12)