SCIENTIFIC ABSTRACT D.F. CHEBOTAREV - G.A. CHEBOTAREV

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R000308220007-9
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: June 12, 2000
• Sequence Number: 7
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

NISTMIOT. A.I.---(continued) Card 21.
2. Chlenv-korrespondentv AHN SSSR (for Dolgo-Saburov.
Chumikav,
Zhdanov, 'Jir3nikov, Sokolova-Ponomrava. Batkis,
Shnelev, Holchanova,
Blokhln, Ioffe, Bogdanov). 3. Direktor Instituta
gerontologii
ANN SM (for Gorey). 4. Direktor Inatituts famakologli i
Iddnioterapii ANN SSSR (for Zakilsov). 5.
Derstvitel'n~vv. chlen
Vuesoy=no3r alcademii sel'sl-okhozvaystvennykh nauir,
imeni V.I.Lenina
(VASWIL); direktor Instituta opidemiologii i
mikrobiologii imeni
Oam-lel ANN SSM (for Murontsev). 6. Direktor Instituta po
izueheniyu poliomiyelita AKH S&rA (for ChurAko-q). 7.
Direlctor
Instituta okeperimentallnoy meditsiny ANN SSSR (for
Birvukov).
8. Direktor Instituta obahchey i kommunal'noy gigiyeny
ANN SSSR
(for Lltvinov). 9. Direktor Instituta pediatrii AMU SSSR
(for
Sokolova-Ponomareva). 10. Direktor Inatituta virusologii
AMI
SM (for Xosyskov). 11. Direktor Instituta tuberkuleza M(H
SSM (Shmelev). 12. Direktor Inatituta grudnoy khirurgii
AHN
-SSM (for Busalov). 13. Direktor Instituta pitaniva AM
SSSR
(for Holchanova). 140 Direktor Instituta
eksperimentallnoy i
klinicheskov. onkologii AIGI SSSR (for Blokhin). 15.
Direktor
Institute. khirurgii ANN SSSR (for Vishnevskiy).

MISMOT, A-I.-- (continued) Card -3.
16. Direktor Inatituta f iziologii AJOI SSSR (for
Chernigovskiy).
17. Direktor Inatituts terapii AM SSSR (for
Myssnikov). 18.
Direktar Gosudaristvannopo izdatelletva maditainskoy
literatury
(for Vavevskiv). 19. Vitse-prezident AHN SSSR (for
Davydovskiv.).
209 Hinistr sdravookhranenivu SSSR (for lurashov). 21.
Direktor
Instituta infektsioWkh bolezney AHN SSSR (for
Bogdanov).
22. Chlen-korrespondent AN BSSR: predsedatel' Uchenogo
maditain-
kopgo soveta Miniaterstva zdravookhraneniya BSSR (for
Bronovit-
M
y). 23- Predesdatel' Uchanogo meditsinskogo sovata
Hinisterstva
bratlaniya USSR (for Chebotarev).
(MIefOr~-

GORIV. NA., prof.; CMMOUM. D.F.,,,_prof. (Xiyev)
Some questIons on the problem or gerontoloa, 111n.med. 37
no.9*.
11-15 S 159. (KM 12:12)
(GStUIRICS) -

TARIV. Dmitriy 16dorovichi prof.; MUMMIKIT, T.T., red.;
GIT~ Ved.
Eluternal pathology In the clinical aspects of
obstetrics and
gynecology] Thutrenniaia patologiia v klinike
akmsherstys i
ginekologil. Kiev, Goe.mad.isd-vo USSR, 196o. 214 p.
(GYNBCOLOGY) (KIRA 13:12)

GHMWTAREV, D.P., pror.
Iffoot or pregnancy on the oourse of various interml
diseases.
Em.med. 24 no*9810-19 9 260. (KM 23sl2)
(PMMUGT, WOUCATIONS CIP)

,,- ~CIMM~AIMV ~16&p Prof.; BALUX&V# S.I.P daktor Md.
zauk
On medicinal substances for--the prevention and
treatme-nt of
prewture aging, - Swe made 24 no. 10.3-23 C) 160o (MM.
13:12)
1. Is Instituta geroutologii i ekaperimentallnoy
patologii ANN
SM.
(GnIATRICS)

CHMMAREV9 DeFe. prof*
For the further develolment of wdical science in the Ukrainian S.S.R.
Vrach.delo no,U:" 1 9600 OCIM 134.n)
1. Predsedatell Uchabnogo soveta. Ministerstya adravockhrananiya USSR.
(URRAMIE--NMICM)

GANDZHA, Igor' Mikheylovich; CIMBOTAFMV, D.F.,
red.; POTOTSKAYA, L.A.,
tekhn. red. 'w-
[Tbe cardiovascular system in diseases of the
liver and biliary
tract] Serdeckmo-sosudistaia sistema pri,
bolezniakh pecheni i
zbelebmvkh putei. Kiev,, Gosmedizdatq USSR, 1961
154P.
iMIRA 15:6)
(CARDIOVASCUIAR SrSM) (LIM-DI=M)
(BILIARY TRACT-DISEA

CREBOTAREV,D.F. [Chebotar~jov,~* D.F.]
Man should have a long life. Nauka i zhyttia 11 no-8:38-44 Ag
61. (MIRA 14:12)
1. Chlen-korrespondent Akademii meditsinskikh nauk SSSR.
(HYGIENE)

GOREV, Nikolay Elikolayevich, red.; 1',ANIKOVSKIY, MI.,,
red.; W4RCHUK, P.D.,
red.; SACHUK, W.N.v red.; FROLIKIS, D.F., red.;
red.; SHURUPOVA, Ye.A.., red.; GOL'SWEYN, N.I.., red.;
LEBEDEVA,
Z.V.., tekhn. red.
[Problems of gerontology and geriatrics]Vopro.V
L;erontologii i
geriatrii. Leningrad, fiedgizy 1962. 279 p. (MIRA 15;9)
1. Akademiya meditsinskikh nauk SM, Moscow. 2.
Deystvitel'Wy cbIen
Akademii neditsinskikh nauk SSSR (for Gorev).
(GERIATRICS) (OLD ACE)

IVANOV, V.N.9 akademikp prof.., otv. red.; BUTRCIMISMY,
G.I., prof.,
zair. red.; LIKIE12181ITall, Ye.l., doktor.med. nauk,
red.;
IUMIEV, A.L... zasl. dayatell nauki, prof,,, red.;
FEUSHCMM, A.P.,, dots.; red.; RENqJTShIY, Ye.L.., starshiy
nauchnyy sotr., red.; SKOPIGHEIIKO, N.F., dots., red.;
P , prof., red.; Y.01011SKIY, D.B., prof., red.;
GITS=Np A.D,I, tekhn. red.
[Transactions of the 7th Congress of Therapeutists of the
Ulcrainian S.S.R.]Trudy VII s"ezda terapevtov Ukrainskoi
SSR.
Kiev, Gosmedizdat USSR, 1962. 610 p. (141IRA 15:10)
1, S"yezd terapevtov.Ukrainskoy SSR. 7th, 1957. 2.
Akaderdya
naulc Ukrainskoy SSR I deystvitellnyv. chlen Akaderii
meditsin-
skikh nauk SSSR, predsedntell Pravleniya Respublikanskogo
nauchnogo obshchestva terapevtov Ukrainskoy SSR (for
Ivanov).
3. Glav?Wy terapovt Ilinisterstva zdravook-hranoniya
IJkxainskoy
SSR (for Chebotarev). 4. Otnt"venW aftre6orl Prawleniya
nauabnogo ob~Mkkeatva terape-vtov ljkrainskoy
SSR for Revutskiy). 5. Zamestiteli predsedrtelya
Pravleniya
Respublikanskogo nauchnogo obshchestva terapevtov
llkrainskoy
SSR (for I-Liklmev, Chebotarev).
(THMINFEUTICS-CO11GRESSES)

GOREV, N.N., red.; FROLIKIS, V.V., red.; red.;
SHURUPOVA, Ye.A., red.; VERKHR.ATSKIY, N.S., red.
[Mbehanime of aging) NlekhanizxW stareniia Kiev,,
Gos.med,
isd-yo USSR, 1963. 499 p. (MIRA 1601)
1. Akademiya maditainskikh nauk SS!M. Moscow. Institut
gerontologii
i sisperimentallnoy patologli. 2. Chlen-korrespondent
ANN SSM
-Xfor Chebotarev). 3. Institut garontologii i
eksperimentalln6k
patologii AHN SSSR (for Verkhratskiy).
(GMIATRICS)

CBEBOTAREV, D.F., prof. (Kiyer)
Current problems in gerontology and geriatrics.
Sov.med. 26 no.29
8-17 F163. (MIM 16z6)
1. Iz Instituta gerontologii i eksperimentallnoy
patologii
AIM SSSR. Chlen-korrespo~dent AIT SUR.
(GMIATRICS)

CHEBOTAREV, D.F.; SACHUK, N.N.
Medical and sanitary survey on old persons in the
U.S.S.R. Vest.
AMN SSSR 19 no,6.*18-23 264. (MIRA 1814)
1. Institut gerontologii AMN SSSR, Kiyev.

CHEDOTAREV. D.F.: KORKUSHKO, O.V.; SACHUX, N.N.;
VOIDSHCHENKO, I.I.
Some data on atherosclerotic cardiosclerosis in very
old persons.
Vop. geron. i geriat. 4:159-166 165. (14IRA 18:5)
1. Institut gerontologii AMN SSSR, Klyev.

CHEBOTAREV, D. N.
"Ifechanization of Soil I;ork.." Byul. Stroi.
tekh., 9, No. 11, 1952

1. CHEBOTARMS D.N.
2. USSR (600)
4. Road machinery
7. Improving the c4truction of a scraper blade. B~L. stroi.tekh.
9 rio. 21 1952
I=. , n Up- -
9. Monthly List of Russian Accessions. Libr=7 of Congress, I .
hj.,,j953,%.U cgLfied.

CHOWAREV, D. N. I KOGAN, M. 0. Engs.
Ditches - --I .
Use of stock material for bracing ditches. Strai. prom. 30 no.
5', 1952
Monthly List of Russin Aeggesions, Library of Congreseq
September 1052. UNCLASSIFIED

CHEXTAREEVJ D. N.
"Some Problems of Lork- Organization in Granite Quarries,"
St-roi. Prom., 30, No. 8,
1952o

C11,201: --I..".,.'Ar) 1". IN. , Eng.
Pile Driving
Suggestion for tho rapid r.--twidng of a woodQn pile with the
concret.,.~ bi't-; er 1-37
Biul. stroi. tekh. 10, No. 5, 1Q,53-
Monthly Listu of Russian Accessions, Librarv of Con-ress, June
1953. Uncl.
. I

1. CHEBOTAREW, D.N.
2. USSR (600)
4. Hydrants
7. Altering the construction of fire hydrants, Biul.stroi.tekh.
10 no. 7, 1953.
9. Monthl List of Russian Accessions, Library of Congress, APRIL
1953, Uncl.

CMMOUM, D.N.. inshener.
Brasklag up from= gromd an bulldlag @Item, Strel.
promo 33
n0.9:6-10 3 155, (KE8A 9:1)
(Frozen ground)

MLUKOV, N.F. (Darikov); LYSHKMCH, V.A. (Kharlkov);
STCROZHEITO, A.A.
(Miar'kov),' CIEBOTABEV. D.N. (Kharlkov)
Concrete piles with a corrugated surface. Oan.,
fund. i mekh.
grun. 4 no.3:17-18 162.' (MIRA 15:7)
(Piling (Civil engineering))
(Precast concrete construction)

Repair of Industrial trucks. Put' I put.khos. 4 no. 5:16
6o. (KIRA 13:11)
1. 2amestitell nachallniks slushby puti, Chelyabinsk.
(Chelyabinsk-4ailroade, Industrial-NaIntenance and repir)

AID P - 2909
Subject USSR/Electricity
Card 1/1 Pub. 26 - 6/32
Author Chebotarev, F. N., Eng.
Title : 'Improving or load curves and demand factors or hydraulic-
fill work
Periodical : Elek.sta., .7, 21-22, Jl 1955
Abstract : The article discusses an efficient manner of utilizing
power in the operation of dredges and excavators.
Hydraulic'earth work at the Tsimlyanskaya Power Devel-
opment is reported. The planning of earth work is
explained in detail and a table gives types and
capacities of different dredges and pumping stations.
One diagram.
Institution : None
Submitted : No date

BOGDAMN, T.ia.. lashener; WO IMM, AX, lushener;
CHROMAUF, FX,
lushoner. pgs-~-
bwrove the equipment uA toohnoloa for by&aullo
mining* Mahe
tidiLrab 9 no*10:27.29. 0 1559 (KUU 9: 1)
. (Hydrualic minim)

CHEBOTAREV. G.A.; BOZHKOVAI A.I.
0
Stability of elliptical orbits in the sphere of action
of Jupiter.
Siul.Inst.toor.astron. 8 no.9s641-646 t62. (MIRA 17:4)

CIIFBPTAU-V., G.A.
Ivan D&nilovich Zliongolovich, 18~12 - 5 on the
occs?ion of his
70th birthday. Blul.Inst.t-or.astron,. 8 nn.9;69~-702
'62.
iNfl.A., 17:4)

CAo,'802A-R~V, G. A., -,'IIUS~ L. YU., U!'M-FJI0VAi yll~- !I.
Orbits
Absolute, periodic orbit of the Hestia type. Biul. Inst. teor.
astron. 5 No. 1, 1951.
9. Monthl List of Russian Accessions, Library of Congress, Aurusi
1952 Yffl, Uncl.

CMMOTAREV, G.ik.
Now determination of the mass of Mercur7.
Vop.koem.1:234-240
152. (Nercury (Planet)) OWRA 7:2)

CHDOTAMV, G.A.
Analytic thsor7 of the notion of Rilda.
no.5:249-270 153.
(Planets. Minor-153)
Blul.lustoteoreastron. 5
(Oft 7:6)

CUBOTAREV, G.A.
-
Avolution of orbits In the Inner area of the
asteroid ring.
Biul.Inst.teor.astron. 5 no.7:393-411 '53, (NLRA
7:5)
(Planets, Minor)

CHEBOTAREVO 0. A.
BMILZWUIY, V.T.; CMMOTARN, G.A.
.
"0"'0W
Ellussian technical literature of the first quarter of
the 18th
contm) Ras*W& UkhatebodWa 11toratura pervol chetvortl
M11 vska. Moskva, lad-vo Akedeall nook SM. 1954. 358 p.
(Techablea-Blatory) (MraA 7:7)

CMUOTARIT, G.A.; BOZHKOVA, A. I.
Brolution of orbits of minor plawts of the Hilda group.
BluMnste'
tooreastron. 5 noo9:571-593 154. (KERA 8:4)
(Pla=ts, Ninor) (Orbits)

CHEBOTARIV, G-A-; WZHIOVA9 Aol-
Theory of notion of the TroJau gro'QP of asteroids.
Blul. Inst.
teore astrone 6 noel#S221-231 '55. (NM 13:3)
(Planets. Minor)

ILTKMUYAO A.K.i SKIRMOVA. V.L. akademik. redaktor;
CIM ANIVA G.A.,
dokto,? 'fist ko-sm tematt cheskikh nauk,
otvetstvain j. ~rmg W.
PlTZM, B.S.. tekhaicheskly redaktor
[Bibltographical index to U.S.S.R.*pubUcations in
mathematics and
mchaocs from 1917 to 19521 Bibliografleheskis
ingtochniki p* 0
=texqtike L wkhanike, izdansWe v SSSR sa 1917-1952
gg. Sost.
A.K.Likoneksta.'Vod red. M-Sidrnovs. Koskva, 1957.
354 p.
(KLRA 100)
I* Aicadenlya nauk S33R. Biblioteks, 2. Direktor
Bibliotaki
Akedeall nauk SSSR(for Chabotamv)
(Dibliograpby-Kathematics) (Bibliograpby--Keehanies)

POR#MALI V.B HATANSON, G.I.; ALMMNMA. V.P.; SKIRNOY. V.I..
skademik.
red.; CHOWARIV, G.A., prof,, doktor f is 1ko-mm tome
ticheakikh
nauk, ZXBU' R.N.. tekhn.rod.
EMathematics ana z9obsuics, in the publications of the
AcadeW of
Science of the U~5,3.1e; a bibliography] Natematike i
mekhanike v
Isdanitakh Almdamil mauk SSU; bibliogrof i1a. Sostavili
T.DePortugell,
G.I.Nistanson. V.PAleksopova. Pad red. V.I.Sairnova.
Moskva* TOW.
1948-1952. 1.957. 361 P. (MIRA 11:4)
1. Akaden4a nauk SSOR. Bibliotekse
,bliogrepar-YAtheamtics)
(Bibliograpbr-Mochanics)

SOV/124-58-1-46
:Translation from: Referativnyy zhurnal, Mekhanika, 1958~ Nr 1, p
6 (USSR)
AUTHOR: Chebotar
TITLEt A Symmetrical Trajectory tor a C"r, R~,%J ct(Simmetrichnava
trayektoriya rakety dlya poletd vokrug Luny)
PERIODICAL: Byul. In-ta teor. astron. AN SSSR, 1957, Vol 6, Nr 7,
pp 487-492
ABSTRACT: The author determines the initial conditions of motion
for a rocket
which, upon departing from the surface of the Earth at. the time
t~0,
is to circle the moon and return to the Earth; no con5ideration
;.s given
to the drag of the Earth's atmosphere upon the motion of the
rccket..
The author starts out from the follov-.-ng concept. Let at some
moment
of time to the moon and the rocket be located on the x ax-s
whereir,
the distance of the rocket from Earth xO ".-- grea!er-~!-~,.n
'tnt 01stance
of the moon from Earth xo and the velocAy of the rocket is zero,
If
the gravitational attraction of the moon were not considered,
then the
rocket would approach the Earth along the x axis, The lunar
disturb-
ance will deform the rectilinear trajectory of the rocket so
that, in its
motion from the point xo, it will puss at some distance rmin irom
the
Card J/? center of the Earth. This lunar disturbance will
decrease as the

A Symmetrical Trajectory tor a Circurniuva, RcJet
SOV/124-58, 1-46
nuantitv A0 ~ 0 .- 0 - 1 4
x XI is increased. Thus, a su able selection of this aL. ntitv
may
r. c n (.1 e rrMin < R, where R is the rddius of the Earth. if
the motion ol, the moon
is imagined. io be in the opposite sense, then the rocket, in
its motion from tbe point
X0, will describe a new trajectory which is svmrnetr,;cal to
the one Just described.
T',-~_c position and velocity of the rocket at the moment of
its reentry Yield the irit'.al
cond-Aion~ that are required to launch the rocket to the
position x". The imagined
eversed motion of the moon is then replaced by its natural
motion. A 0 is asst:med
to cquA 15,600 km as a first approximation. The numerical
integraton is pe:forrried
hy Coxve)_~ s method, using a one--hour integrati.on. interval.
For t > 100 hTS the lunar
S: Are found to be insignificant, and tny further-
motion5,,.xre considered as
Tn that case rMin is found to equal 32,975 km, ;. e, , the
rocket will
P_ss at _'b, 597 km from the surface of the Earth,. In a second
approximation Ao is
set, ai-31,600 km, and a two--hout integration interval is
used; rmin is then 5.619 km.
T~-.e re-ent-y conditions are found from the eq-udtiOn
T=R:;6,.378 km. The initial condi-
i;ons ior the circumlunar flight are determined by the
parameters a=215, ZOO km,
M -:0(': 1 t,'e-4.97598, and ir :--1830.18. The initial speed
will be 11,080 m/sec. The
toia' duration of the flight of the rocket will be 236.14 hrs.
The minimum distance
rocket from the suriace of the moon will be 29,860 km.
V. S. Nox,oiielov
Card '212

C ,,10
AUTHOR: Chebotarev, G. A., Doctor of Physico..Iiathematical
3o-9-16/48
-Ze-rences _.
TITLE: An Act of Friendship4 - Me lbopening'of the Gotha Mbzw7
(Akt druzhby.- Na otkrytii Gotskoy Biblioteki).
PERIODICAL: Vestnik AN SSSR, 1957, Vol. 27, Nr 9j pp. 69-9o
(USSR)-e
ABSTRACT: The famous library of the city of Gotha was after ten
years of
preservation in the USSR returned to the German Democratic
Republic.
The author of this report describes the short ceremony in which
he
personally participated. The official return took place in the
hall
of mirrors of the castle of Friddenstein (Fridenshteyn) in the
pre-
sence of renowned personalities of the German Democratic
Republico
The library belongs to the most precious collections of Germany-
(more than 3oo-ooo volumes). German histary is especially
extensively
represented and without any gap the library comprises Ge-,.An
publl-
cations from the XVI ti.U into the M century. The geographic sec-
tor is also richIv represented. About half of the collection
consists
of works which were published till the XIX century, among then
prom
cious paleatypes: the famous Luther-bible (1521) and a rich
collece
Card 1A tion of Lutherean original sciptsq

-4
An Act of Friendships - The Fbopening of the Goths Library.
3o-9-16/48
There is Ifigure.
AVAVABLE: Library of Congress*
Card 2/2

CERBOTAM, G., doktor fjsjkv-mtevmticbssklkh wLuk.
professor.
Coamle boomrang* Zma.vila 32 no.2:28-29 7 '57o (Km
10:5)
(Interplanetary vorwa)

H F- 1~ TAK F V
ISACHINKO, A.I.; SHAIRANOVUIY. K.I.; RAYDONIKI, V.S., red.;
CFd1BOTiR1V. G.A.
otvatstvenW red,; LUPPOT, S.P., otvetetvennNy red.r~.-i't-S.,
takhnerade
CNIthall AvAr"vich ~Mtelen; a bibliography] Mikhail Andreevich
Shatelen: bibliogrefichaskit ukazatell. Uost. A.I.Isachanko, K.I.
Shefranowskil. Pod redo V.S.Rovdoulks. Koskvn. 1958. 198 p.
(MDU 11:4)
1, Akedmiye nook WO. Biblioteks.
(Bibliographr-4hatelen, Mikhail Andresvich, 1866-19-57)
k

XAMOGRADSKAYA. 0.P.; YIJIROV, K.Y., prof.,doktor
khim.nauk. nouchnyy
red* [deceased]; CH39BOTAFM G.A.. oty.red.; ARON.
G.K.. red.
Izd-va; SKLMOTA, ioid.
(Chamical literature of ths U.S.S.Rj ZhIsichaskals
literaturs,
SSSR. Tol.l. No03 Echomistry In pablications of the
AcadeiW of
Sciences of the U,S.S.R.. 1936-29371 Wails v
isdanilakh Alademil
nauk SSS16 1936-1937. Sostavila O.P.xamenogradsk&ia.
Prodiel. I
nauchn.redA.T.Flerova,* Kookwa~19580 568 p. (MIRA
12:3)
Is Akadenlys nauk SSSR, Biblioteka.
(Bibliography-Chemistry)

CHEBOTAREV, G. A. !e
Annual ~Ieeting of the Aead. Sci. USS. Priroda, 1958, No. 5,
pp. 105-107.
The annual meeting of the Ald, Nauk SIM, was devoted to Soviet
Acheivements In science and technics in 1957, as well as
cur-rent and future projects.
The following achievements in the development of
geolo-geographical
science,were recorded:
"Organization of the Novosibirsk East Sectim of the Library of
the AS USM."

~ - CMMOTAFW.. G.A.
Matallia Sergesym Samollova-Ifthontova, (on the
occasion
of her 60th birthday). Btul.Inst.tsor.astroue 6 no,9:
675-680 158. (MIRA 130)
(Samollova-Ifthontova. lataltia Sergesyna, 1896 -

ITM

AUTHORt
ghabalw_svp G.-A., Doctor of Physical
SOV/30-58-12-17 /46

and Matheasti-da-T-Sci*nces
TITIZe
400th
Anniversary of the University of Jens (400-lftiY*

Iyouskogo
universit*ta)
MIODICALs
Vestnik Akadeaii naltl- SSSR, 1958,
Nr 12, PP 69 - 70 (USSR)
ABSTRACTs
The University of Jena has
a rich tradition, particularly

in the field of natural and
medical sciences. During the

Second World War it suffered
heavy damage, which, however,

could not prevent its being
reopened on October 15, 1945.

At the ease time its
reconstruction was begun. The anniver-

sary oolebrations
were attended by scientists from many

countries. The Soviet
Union was represented by delegations

of the AS USSR, the
Minist*ratvo vysahego obrazov&niya

(Ministry of ligher
Education) and the Ministerstvo

I V "Iffil 0-1- SSSR
(Ministry of Public Health, 'USSR). on

September
3, onorary doctor's diplomas were awarded to

German and
foreign scientists. DLplozas were handed over

by the Taculty
of Mathematical and Natural Sciences to the

loader of the
delegation of the AG USSR, D. I. Shcherbakov,
Card V2
Academician, to be forwarded to A. N. Neemeyanov and A. I.

400th Anniversary of t4p
SOV/30-58-12-17/46
Oparin, Academicians. The Faculty of Agriculture bestowed
diplomas on N. V. Taitain, Academician, and the Faculty of
Philosopby on the-author of this article. The rectors con-
ferenoe of the Test German Universities decided not to attend
this celebration. The Soviet Scientists hold lectures in
Jena and in some other towns on scientific and cultural
achievements in the USSR. There is 1 figure.
Card 2/2

MICKSKAYA F'A.K.; CMIBOTAHNT, G.A.. oty.red.; DORMAN,
YO.G.. Prof.,
red.; ARM. -0.1t. red'Asti-va; PJIVZIDM. B.6.. tokhn,red.
[Principal foraism bibliographical sources for physics,
1931-19551 Osnovve InostranVe bibliografichoside
IstochnIld po fialks. 1931-1955. Soot. A.K.Inkounksla.
Pod red. MG.Dorfmam. Mosima, 1939, 114 P. (NIRA 12:6)
1. Akadeviya a&uk SM. Bibliateka.

69848
C. 0 SOV/35-59-9-6929
cl /sIS-0
Translation from: Referativnyy 2hUrnal, Astronomiya i Geodezlya,
1959, Nr 9, pp 8 9
(USSR)
AUTHORS.- Chebotarev, G.A., Bozbkova, A.I.
TITLE: The Study of the Motion of Two Trojans by the Numerical
Method
PERIODICAL: Byul. In-ta -teor. astron. AS USSR, 1959, Vol 7, Nr 3,
pp 186 - 201
(Engl.. r6sumfiy-.
A W-Tl-'Aft: The' jAution of two Trojans'has been studied - of
Patroclus (617) and of
Anchises (1173) over a-period of - 710 years. The motion of the
Trojans
in the plane of motion of Jupiter is examined, a numerical
integration
in the rectangular coordinates is carried out by the Cowell
method, and
only the perturbations from Jupiter are allowed for. The motion of
Jupiter is considered to be unperturbed and the integration
interval
W - 1 :80 of the complete revolution of Jupiter. Patroclus was
chosen
as the Trojan with the greatest eccentricity and the greatest
inclination,
and Anchises as the Trojan with the greatest daily motion. orbital
elements
of both Trojans are given, calculated after each revolution of
Jupiter. The
Card 1/2 big semi-axis of Patroclus undergoes long-periodic
fluctuations, with the

69848
The Study of the Motion of Two Trojans by the Numerical Method
SOV/3,55-59-9-6929
Period ~ 12.3 revolutions of Jupiter or 146 years, the
eccentricity decreases secularly,
the apside line rotates at an average speed of A6'r - 00.842 per
one revolution of
Jupiter. The big semi-axis of Anchises also has long-periodic
fluctuations with the
period - 12.6 revolutions of Jupiter, the eccentricity remains
constant while the speed
of rotation of the apside line is,07r. +JO.850. In the whole
interval, the joviocentric
orbit of Patroclus retains its elliptical character, while the
Anchises orbit periodically
changes Its character, passing from elliptical to hyperbolical
and back.
N.S. Yakhontova
Card 2/2

69M 47
~13 /1/,;,) 0 SOV/35-59-9- 9
Translation from: Referativnyy zhurnal, Astronomiya i Geodeziya,
1959, Nr 9, p 11 (USSR)
AUTHORS: Chebotarev, G.A., Volkov, M,S.
TITLE: The Motion"'Kf Patroclus in the Gravitation Field of the
Sun and Proto-
Jupiter
PERIODICAL: Byul. In--ta teor..astron. AS US5R, 1959, Vol 7, Nr
3, pp 202 - 207
(Engi. r6sum6)
ABSTRACT: The motion of a small Qlanet-of the Trojan group,
Patroclus, was examined
in the gravitation field of the Sun and proto-Jupiter in order to
clear up
the question on the stability of the motion of Patroclus. It was
assumed
that the motion of Patroclus took place in the plane of Jupiter,
that the
motion of Jupiter was un-perturbed and its mass was 20 times
greater than
the present one; for the daily motion the present value was
preserved.
The numerical integration was carried out during 33 revolutions
of Jupiter.
During this period the radius-vector of Patroclus changes from
3.7 to
7.8 A.U. and the distance from Jupiter, from 1.9 to 11.9 A.U.
After 27 re
volutiormits stability of motion is disturbed and it departs from
the point
Card 1/1 of libration. Bibl. 9 titles. N.S. Yakhontova'

LUXONKAU, A.M.; LOSINAKIT. 5.R.. prof.. md.-, CRIBOUM,
G.A., otv.redo;
KALI q N.M.# red.isd-ye; BOCHXM. T.2. q -U]i ~o"d~e~
-EPrlncipal foreign bibliefraphioal sauroas for
literature an
mothowtice and mchanlose 1931-19571 Onnownya
Inostrannyo
bibliograficbmakle Istodmiki po motemotike I mkhanike,
1931-1957o
Soot. A.K.Lukommkols. Fod rod. S.NoUslaskogo. Moskva.
1960.
181 p. (KMA 14:2)
1. Alcodemlya nouk SM BIbIlotaka.
(B1bl1ograpby-46mth~wt1c*)
(Bibliography-Ykabonica)

_ - --------
4t 85204
31/035/60/000/010/003/021
AOO1,(AOO1
Translation from: Referativnyy zhurnal, Astronomlya I Geodeziya,
1960, No. 10,
P. 9, # 9814
AUTHORS: Chebotarev, 0. A., Bozhkova, A. I.
Vf Circular Orbits Within-the Sphere of Jupiter
TITLE: On the Stabilit? 0
Influence
PERIODICAL: Byull. In-ta, teor. astron. AN SSSR,:1960, Vol. 7, No.
8. PP. 581-587
(English summary)
TEM The problem Is considered on the stability of motion of
Jupiter's
satellites whose orbits are within-its influence sphere or near the
boundaries of
this sphere. Side-by-side with th 14upiter influence sphere the
authors introduce
a sphere with the radius R* = r 1m (ml is Jupiter mass) within
which Jupiter's
attraction Is stronger than that oi the Sun. The motion of six
fictitious
Jupiter's satellites Is considered moving along circular orbits
with semiaxes:
ao - 0.30; 0.28; 0.25; 0.20; 0.15 and 0.10. The integration of
motion
equations Is performed by Cowell's method with six decimals. It is
shown that
Card 1/2

85204
3/035./60/000/010/00V021
AOOI/AOOI
On the Stability of Circular Orbits Within the Sphere of
Jupiter Influence
beyond the limits of the sphere with radius R* the motion along
a circular orbit
is unstable. It Is noted that all the actual Jupiter satellites
are within this
sphere.
N. S. Yakhontova
Translatorts note: This Is the full translation of the original
Russian abstract.
Card 2/2

CH .0 11NAZ V
S?511/61/66 0 4
Bi 63/B1 86
-AUTHORS;
_t G. A.9 and.Volkov,.M.. S.
TITLE: The st~Lbility of circular orbits with retrograde motion in
the sphere.of action of Jupiter
Akademiya nauk SSSR. Institut teoreticheskoy astronomii.
Byulleten.le ve 80 no., 2(95), 1961, 99 102
TFXT: Five~initially circular satellite orbits were computed
numerically
0 - I e initial mome
Edith the following initia1 conditi ns. n th nt, the sun,
J,
ujpi ter. and the satellite are ~axranged along the x axis,
and.-Jupiter is
:in-perihelion position.:. The initialmajor axis.of the satellite
orbit is;
a 0.2, 0.25, 0-3, 0.35, and 0-4 astronomical units respectively.
Since
on of 1)
the sDhere.of acti ,Jupiter,under these conditions is R = 0.2791,
satellites I-and 11 are within the sphere of actionwhile III, IV,
and V
are outsides The numerical computation is carried out with an
accuracy of!
~,six decimal places, and the method is the same as in earlier
pappr.by
G. A. Chebotarev~and A. I.-Boshkova.'_ The integration is performed
for a
time interval of 11.86 years equal to one sidereal revolution of
Jupiter'
-around the sun. The variations,of the major axis and the
eccentricity wiih
Card 1/?

S/035/61/000/011/001/028
A001/A101
AUTHORS: Chebotare 9-A.., Volkov, M.S.
TITLEi On stability of circular orbits with retrograde motion
in the
Jupiter sphere of influence
PERIODICAL: Referativnyy zhurnal. Astronomiya. I Geodeziya, no.
11, 1951, 7,
0
abstract 11A71 ("Byul. In-ta teor. astron. AN SSSR", 1961, v, 8,
no, 2, 99 - 102, Engl. summary)
MXT~ The problem is considered on stability of circular orbits
with
retrograde motion, situated within the Jupiter sphere of
influence (R = O._322 AU)
or close to the boundaries of this sphere. It is shown, by the
numerical inte-
gration method, that satellites with retrograde.motion are
characterized by con-
siderably higher stability than direct satellites: Jupiter's
satellites moving
directly leave its sphere of influence for ever already at a0=
0.20 AD, whereas
in the case of retrograde motion instability takes place beyond
the limits of
the Influence sphere,
[Abstracter's note: Complete translation) N. Ya.
Card 1/1

89328
3,144oo S/033/61/038/001/oll/oig
; AAP 0 E032/E314
AUTHORS: Gontkovskaya, V.T. and Chebotarev, G.A.
TITLE: Orbit of the Third Soviet Space Rocket (Lunik 111)
PERIODICAL: Astronomicheakiy zhurnal. 1961, Vol. 38, No. 1,
pp. 125 - 130
TEXT: The motion of Lunik III in the period October 15 to
March 309 196o, is investigated. The third Soviet space
rocket was launched in the morning of October k9 1159, in
the direction of the Moon. On October 6 at 17 21 Moscow time
the rocket reached a distance of 6 200 km from the lunar
surface.
On October 11 at 00 44M the rocket reached the apogee of its
orbit (480 500 km from the Earth) after which it began to
appr9ach the Earth again. The passage of th~ rocket through
the
perigee should have taken place on October 18 at
19h 49m and the perigee distance should have been 47 490 km.
However, for well-known reasons, the radio contact with the
cosmi.c rocket was lost (Sedov - Ref. 1) and already during
its
first approach to the per'-gee the rocket could not be
observed
Card 1/11

89326
S/033/61/038/001/011/019
E032/E314
Orbit of the Third Soviet Space Rocket (Lunik III)
in spite of favourable conditions and the availability of an
accurate ephemeride (Guntzel-Lingner, Ref. 2). The orbit of
Lunik III is of particular interest from the standpoint of
celestial mechanics. A particular feature of the orbit is
that it has unusual elements (e = 0.98, i = 850) and the
fact that its elements change rapidly as a result of approaches
to the perturbing body (Moon). The information available at
present (other than the TASS communlqu6) consists of a short
note by Sedov (Ref. 3) and the American calculations (Michaels,
Wachman and Petty - Ref. In the present paper the problem
is formulated as follows:
1) the rocket moves in the gravitational field of the Earth,
the Moon and the Sun;
2) all the bodies except the Earth are looked upon as mass
points and the figure of the Earth is taken to be a biaxial
ellipsoid;
3) both the equations of motion of the rocket and the equations
for the Moon and the Sun are to be integrated!, taking into
rA-A 9/11

89328
S/033/61/038/001/011/019
r-.o32AE314
Orbit of the Third Soviet Space Rocket (Lunik III)
"account mutual perturbations. The equations of motion of the
i'Moon and the Sun are of the form:
dirt 0"11+ nil M, Irl-r, r,
- "A3
78-
dl;s ft+.., - rl - rt rl
M, '& - -
d8z .23 r2 + Al f.
while those of the rocket are:
[r +,pj (r - rj) (2)
W
'Card 3/11

89328
S/033/6i/o38/ooi/oll/o19
E032/E314
Orbit of the Third Soviet Space Rocket (Lunik 111)
In the above equations r i and m i are the radius vector
and the mass of the i-th body multiplied by the gravitational
constant; subscripts 0, 1, 2 refer to the Earth, the Moon
and the Sun, respectively; A ij are the distances between the
bodies; is the radius vector of the rocket; the equations
are written down in the geocentric equatorial system of
coordinates. The term F in Eq. (2) represents the attraction
due to the Earth. The basic characteristics of the terrestrial
ellipsoid are represented by the quantities m, n , which
are related to the equatorial radius as the compression a
and the angular vlocity w of the ellipsoid by the formulae:
2 (1 + it) Go
H~=-s J3 + it) am LC i. - W
Card 4/11 n M - MOV'16-. (3)

d 93 28
Orbit of the Third Soviet Space S/033/61/038/001/011/01.9
Rocket Munik III) E032/3i4
The components are 'given by:
F,, (R - Tv) zel-,
FV (R - Tv) ye,',, (6y
F, (S - Tu)zel-.
where:
3(k+l)ak,
m -3
3 (4y
S=myj(-I)kg7-,k, T=
3P
Card 5/11

89328
Orbit of the Third Soviet Space S/033/61/038/001/011/010,
Rocket (Lunik III) E032/E314
and:
2
u r2 + zv v u (5)
These equqtions can be transformed into the lunocentric
coordinate system in which the equation of the rocket is given
by:
drP. M,
Ma- + + V.- (P- - -p!)
FAp p.3 P32
Ml
-[P+V.(P-pj)l.
PP P 3=0.: ~j3
In this equation:
Card 6/11

89328
S/033/61/038/001/011/019
E032/E314
Orbit of the Third Soviet Space Rocket (Lunik III)
r - rls eo Fil P2 = F2 - Tri
The quantities of .1 and Le respectively represent F and
W in lunocentric coordinates. Numerical integration of
these equations yk1ded the results given in Table 4, the key
of which is as follows: 1 - date; 2 - M, deg;
3 - a(l - e), km; 4 - October; 5 - November; 6 - December;
7 - January; 8 - February; 9 - March.
Fig. 2 shows the variation in the eccentricity of the orbit,
Fig. 3 shows the variation in the perigee distance and
Fig. 4 shows the variation in the inclination of the orbit.
It was found that the effect of the compression of the Earth
on the motion of the rocket lay within the limits of accuracy
of integration. There are 4 figures, 5 tables and A)
6 references: 4 Soviet and 2 non-Soviet.
Card 7/11

89328
S/033/61/038/001/011/019
E032/E3141
orbit of the Third Soviet Space Rocket (Imnik 111)
ASSOCIATION: Institut teorgticheakoy astyanomii Akademii
nauk SSSR (Institute of Theoretical
Astronomy of the Academy of Sciences, USSR)
SUBMITTED: October 7, 1960

S/033/bl/030/001/011/019
E032/E314
Orbit of the Third Soviet Spqce Rocket (Lunik III)
Table 4:
TaGazza 4
3ammmu op6mm pai H mmummall pawm-

rp".
t a Max.
1
a a NA
1 .

1

WA

WA
Is.? OUT.
0.51
182.03
73.84
251.81
79.97
-964 BW
0.824
46640
482 900
3.7
monG.
0.40
WAS
74.44
25t.79
80.99
270 MO
0.839
43 5tO
497 ODO
20.0 nonG.
1.62
184.25
76.44
252.19
84.02
268 30D
0.956
38440
494 200
5.9 A01C.
0.93
184.58
76.91
252.33
84.48
270 40D
O.8a2
31 940
508 900
22.5 AM
0.80
180.02
77.45
251.43
a2.93
269 900
O.9D3
26060
513800
6.7fillB.
0.67
184.60
75.70
25t.tt
83.09
261 BOO
0.924
19 830
502 800
22.4 nun.
0.40
t85 Of
75 18
250
74.37
267
100
0.933
17 890
516 201

~:P
0.02
183:72
76:02
252:
57.95
293 800
0.950
14'170
553 500
25.8
,:
0.35
184.22
75.12
250.
48.00
292.100
0.951
t4 29-0
570 100
14.6 mapT
0.29
t84A7
74.02
24%
47.75
M 500
0.955
t3 030
57t 900
30.7VAPT
359.00
t8U.57
70.38
249.
56.85
270 100
0.980
5 350
534 800
Card 9/11

89328
S/033/61/038/001/011/019
E032/E314
orbit of the Third Soviet Space Rocket (Lunik III)
Fix. 2: Fig. 38
-- - ------- ......
4SAV -
NM-
OAV
me
is no so AM V zu /'is Xs t
Pue. 3. Mmettenne nepureAwra weTonmix TmbeA conemoft
lKOCMllq(!Cxofi pamem
Card 10/11

89328
S/033/61/038/001/011/019
1;032/E314
Orbit of the Third S~viet Space Rocket (Lunilc III)
Fig. 4:.
Pue. 4. llameneutte u&xmseumm0PGMTU TPM.efi
Card 11/11 coneumosl 'roemnqecxA paHmu.

89329
3/yoo
3*0
AUTHORS:
TITLE.
s/o33/61/038/001/012/019
EO-32/E33L4
Brumberg, V.A., Kirpichnikov, S.N. and
Xhobotarov, G.A.
On the Notion of Artificial Moon Satellites
PERIODICAL: Astronomicheskiy zhurnal, 1961, Vol. 38, No. 1,
PP. 131 - 144
TEXT, The launching of artificial Moon satellites is a
probiem for the immediate future. it is known that a number
of attempts have been made in the United States to put a
satellite into orbit round the Moon, although all of them
are said to have been entirely unsuccessful. The theory of
motion of artificial Moon satellites has been widely discussed
in Western literature (Buchheim - Ref. 1, Kooy - Ref. 2,
Kboy and Berghuis - Ref. 3, GrObner and Cap - Ref. 4 and
ThAring - Ref. 5); in Soviet literature the theory of motion
of these satellites was considered by Yegorov (Ref. 6) and
Aksenov and Demin (Ref. 7). Prolonged observations of
artificial Moon satellites may be of great interest from the
point of view of celestial mechanics, since they can be used
Card 1/14

89329
S/033/61/038/001/012/019
E032/E314
On the Motion of Artificial Moon Satellites
to improve the present data on the figure and mass of the
Moon.
The aim of the present paper is to investigate the motion of
Moon satellites by considering a number of special cases, the
solutions being obtained by numerical integrations. From the
mathematical point of view the problem is reduced to the
integration of equations of motion of a mass point having a
negligible mass, moving in the gravitational field of the Moon
and subject to perturbations due to the non-spherical Moon and
the gravitational attraction of the Earth and the Sun. The
motion
of the artificial Moon satellite is described in terms of the
Tean anomaly M I the area vector ~ and the Laplace vector
f which are defined byz
- - t
c = r x r
(5)
Card 2/14

89329
S/033/61/038/001/012/019-
E,03 2/r,,3 14
On the Motion of Artificial I-loon.Satellites
and:
m r
f r r r-(;:rr) o (6)
where is the lunoceniric radius vector of the satellite.
The Moon is assumed to have the form of a uniformly rotating
homogeneous triaxial ellipsoid and the perturbation is
represented in the form:
r, 4p, - r (I + Tj)j + grad V,
The.principal set of coordinates xyz is chosen to be the,
lunocentric system oriented along the principal axes 6f t~e
ellipsoid of inertia of the Moon for the epoch 1960.0-; In
Card 3/14

89329
S/033/61/038/001/012/019
E032/E314
On the Motion of Artificial Moon Satellites
the derivation of the transformation formulae for this system
of coordinates it is assumed that the Moon modes in accordance
w�th the Cassini laws. The physical libration of the Moon
is neglected. The initial instant of time is chosen to be
t = 1960, October 24.0. At this instant the Iloon is in
0
the neighbourhood of the perigee and is in the first quarter,
which may facilitate the observation of the satellite from! the
Earth. The unii of time is one day and the unit of length is
10 njean radii of the Moon. -The other initial data assumed are:
329390,
+
81.375,
Pilo
N
il.~ - (38)
127 12166C'9'~
p =0.272 274 p
Card 4/14
= 6378.270 Kx,

89329
s/o33/61/038/001/012/019
E032/E314
On the Notion of Artificial Noon Satellites
w
here
I is the mean equatorial radius of the Earth,
is the radius of the ?-.oon,
in0 M land m 2 aria the masses of the Eloon, the Earth
and the Sun, respectively (multiplied
by the gravitational constant) and
N is the average angular velocity of the Moon
around its axis.
The initial positions and velocities of the Earth and the
Sun iii the principal system of coordinates xyz have the
following values:
Card 5/14

89329
S/033/61/038/001/012/019
E032/E311k
On the Motion of Artificial Moon Satellites

xx = OJ28 077 44-102.

Y, = 0. 167 612 08. tot,

:, = 0.245 209
82-101,

xt = 0.128 601 29-1041,

Yt = 0.844 314 33-104,

= 0.118 582
14-103,

= 0.418 764 47-101,

91 = 0.325 042 31-101,

"I = - 0.839 719
12. t0-2,

k2 = - 0.143 319 51-103,

g2 = 0.229 757 57-10!,

2 = 0.334
423 30. 10t.

The
initial distribution of the Moon, the Earth and
the Sun

at
the initial instant of
time is as shown in Fig. 2.

The
following four orbits
of the satellite are then computed:

1)
polar
orbit with small eccentricity (Cp) ;

2)
equatorial orbit with
small
eccentricity (Ce)

Card 6/14

89329
S/033/61/038/001/012/019
Un the Eotion. of Artificial Noon satellites
3) polar orbit with large eccentricity (Ep);
4) equatorial orbit with large eccentricity (Ee)
For polar orbits (Cp, Ep) at t it.was assumed that:
0
0 0
90 0 17103'40 (42).
The'quantity was found from the condition that the.
of nodes for the satellite orbit is perpendicular to the
direction of the Sun. For the equatorial orbits (Ce, Ee) it
was assumed that;
0 0
0 + 171 340
Table 1*gives the sununary of the initial data (key to table
1:- 1 - element; 2 - type of orbit.)
Card 7/14

89329
s/o33/61/038/001/012/019
E032/E314
On the Motion of Artificial Moon Satellites
Table 1: 1
Ton op4mu Tyr-
MOW Cp Ep
Card 8/14

0.13528276-100
0
0.18M27-10o
0
~y
'0-10191-879-10~
0 0.12150144-101

0
C,
OA0312460- 101

0
0. 12M275. t~~
f, J
-0.12010540401 1
-0.126J0540-101
-0.46925243-101
-0,46925?43-10t

0.19207686-10-
-100
0. 71473935. UP
0.71473935-10-

h.
0
0
0
0

0
0

89329
S/033/61/038/001/012/019
E032/E314
On the Motion of Artificial Moon Satellites
In the above table, M is the mean anomaly of the satellite.
The initial values of the elements were found for orbits with
low eccentricity from the condition:
hp 500 km, ha 1 500 km (44)
so that: a 0.157 582 56, e 0.182 705 98 (45)
For orbits with large eccentricity the corresponding values
were:
hp ='500 km, ha = 10 000 km (46)
and:
a a-0.402 30841, e = o.679 869 28 (47).
The quantities h p and h. denote the height of the pericentre
Card 9/14

69329
S/033/61/o38/ooI/oI2/oI9
E032/E314
On the Motion of Artificial Moon Satellites
and the apocentre at the initial instant of time. Finally,
the mean anomaly M was chosen to be zero, i.e. at t 0 the
satellite was at the pericentre of its orbit. The integration
of the equations of motion was carried out by the Runge-Kutta
method. 19 equations of the first order and one time equation
were integrated. Table 3 gives the initial and final elements
of the orbits (key to Table 3; Title - Change in orbit Elements
of the Satellite; I - type of orbit; 2 - number of revolutions;
3 a (in lunar radii)-, T (in days); 5 - Cp; 6 - Ce;
7 Ep; 8 - Ee.)
Fig. 3 gives the variation of the eccentricity with number of
complete revolutions. Fig. 4 gives a similar plot for the
quantity cos i and Fig. 5 gives the variation in the distance
of the pericentre (in lunar radii).
Complete numerical data on the basis of which these graphs were
plotted are reproduced. The authors intend to continue their
work in this field.
Card 10/14

89329
8* f7
s/o33/6.i/o38/001/012/019
E032./F,314
on-the Motion of Artificial Moon Satellites
There are 5 figures, 7 tables and 8 refcrences:. 3 Soviet
and 5 non-Soviet.
ASSOCIATION: Institut teoretichaskoy astronomii Akademii.
nauk SSSR (Institute of Theoretical Astronomy
of the Academy of Sciences, USSR)
SUBI-11'r.rED: October 22, 196o
Card 11/14

89329
S/033/61/038/001/012/019
E032/E314
on the I-lotion of Artificial itoon Satellites
,rable 3: Hmmmume wwmeffma OPGWT CUYTNRMIN .11yum
C-1
Card 12/14

4F-)
Tan op5mm

vial)

no.inpuaft OPGHTA
eu-
u mi
0
1

1.57. 1
O.W971
900.OOD
I
MO.= 1
0".0W 1
0. 14 87
c manu
x
TPUCHIreTom
40, 1
1.57521
0.18175
190-.00
1 ~~.8%1
17V.354 1
45-.754 1
0.1487,

Ilan

:)I~ 'IL
manw,
0
0
Ft57-%
FO.181-71 1 0-.000

1 - I
1
0--0001 .0.1487
-

31;CIXCIITPHCIITC-

40 - 1

1.57561 0.173-15 1 0-.W0j

14-.3Wj
o
160 ALL

G-.0101 0.11.88.

TOM

0 1
02311 0.67987 19D-.0001 0-.00d
4

171'.340
0-.00D I 0-GM

,
lml=
on~Ta

.
,

t.
.,
1
I[CUTOTOM
ItCHT

40
1

4
02471

0
68036188-
tO4l8-.4t4l

t7t'.057

117'.6951 O.W72

P
.
.
.
.
.

:)H111)T0j),,a,,,,Ha,,
0
4.0231
10.67987 1 0'.OMI - I

I
0'.WO
I O.M
, ,
PUnT1

1 u ameltenTP11.
l!"'ITICTOM
40
14.0205
1 0.65635 1 1-.539117-.953

1160-.631
1 W.370
I
O.W7(;

89329
S/033/61/038/001/012/019
E032/E314
on the Motion of Artificial bloon Satellites
Fig. 2: Fig. 3:
Tepmumomap
Polar ev&
C17
iv
Pue. 2, Bunmiam pacummomenne 3ewaii,
CM11111ta 11 CHYTHIM AY)IM 3 HA'IafiLVUfi NO
UCItT
Cnrd 13/14
Pue. 3. flameuenue 3xcqpnT ptirv
A.-vot opGnT Cp, Ce, Fp,

89329
S/033/61/038/001/012/019
E032/E314'
On the Motion of Artificial Moon Satellites
Fig. 4: Fig. 5:
tell
Ep
u
u
ATA
.;&.jtzjt Pne.'S. Hameneme peecioxamm nepst
PJIC. 4. 11311eneume xocnnyea llnKnOll- ge-pa (a paAffYcal JIYHM) A-
OP6"T
IJOC-nj X-10 OpGIIT Cp. Ce, Ep, Ec Cp, Cc, Ep. Ee

308
S/033/ql/038/005/011/015
E032/E4 14
AUTHORS: Gontkovskaya, Y.T.,.Chebotarev G,tA*,-,
TITLE: Lunar and solar perturbations-in the motion of the
third Soviet space rocket
PERIODICAL: Antronomicheakiy zhurnal v.38, no-5, i~6i, 954-96o
TEXT: The authors report the results~ of a numerical integration
giving separately the effects of'lunar and solar perturbations in'
the motion of the third Soviet space rockef. The oblateness of
tfie, Earth was found to'have a negligible effect. The
differential equation for the motion of the rocket in the
gravitational field of the Earth and*the Moon, neglecting the
solar perturbations, in taken to be of the form
d2r jr + T, (r - r0l,
where r in the f6dide vec, toro e'rocket, is the radius
vector of the Moon, mo is the mass of the Earth and' al is the
mass of the Moon. The right-hand side is then expanded so that

30823

S/033/61/038/005/011/015

Lunar and solar perturbations

E032/E414

CO
(2k

cc.-IIIq
(12

ri

Finally, the
equations describing the

geocentric motion of
the

Moon and the
Sun including mutual per

turbations are taken
to be
of

the form

Ir-ri MO+-1

r1
7-
(3)

d2 r.3 nto + -2 r + III,
-

r, - r2
-
3

4)

TJ2

r
,

'A

where and m2 are the radius ve
r2

ctor and the mas'v of

the-Sun

Card 2/#-,'?

3082
5/033/61/03605/011/015'
Lunar and solar perturbations ... E032/13414
4612 Ad2l is the distance between tile Moon and the Sun. The
initial instant of time was taken to be October 15, 1959,
15hoom.
The integration of the equations was carried-out by the
Runge-Kutta
method. The results are illustrated by Fig.1 to 4. There are
4 figures, 6 tables and 6 'references; 3 Soviet-bloc and 3
non-Soviet-
bloc. The references to English language publications read as
follows: 7
Ref.l: Y.Kozai, Smithsonian Institution Astrophysical
Observatory,
Research in Space Science, Special Report, No.22, March 20,
1959;
Ref.2: E.Upton, A.Ba 'ilie, P.Musen, Science, V.130, no.3390,.
1710-1711, 18 Dec. 1959;
Ref.3: M.Moe, Astron. Roy. SOC. J., V-30, n0.5, 1960..
ASSOCIATION: Institut teoreticheskoy astronomii Akademii nauk
SSSR
(Institute of Theoretical Astronomy AS USSR)
SUBMITTED: January 20, 1961
Card 3/0 -7)

CHEBOTAREV,..G.A., prof.
Publication of the issue no.10D of "Biunsten' Institute,
teoreticInskoi astronamii.0 Biul.Inst.teor,estron. 8
no.7:457-458 162. WRA 15:9)
1. Otyetstvonnyy redaktor Byulletenya, Instituta
teoraticheskoy
Astronanii.
(Astronomy-Periodicals)

MrACHINO V.F.; CHkTTAREY#- G
,A., otv.red.,.prof.; GOLISHTEYN, G A.9
red,izd-va; SOROKINA, V.A., tekhn.red.
[Estimating the error of numerical methods for the
integration of
e4uationo of celestlal mechanical Otsenka pogreshnosti
chislennykh
metodov integrtrovaniia u*inerdi nebesnoi wkhaniki,,
Mogkva, 1962.
537-639 p. (Akadeaiia nauk SSSR. Institut
teoreticheskoi astranomii.
Riulleten'. vol.8, no.9). ()UPA 170)

El" X, K.I.; CHNSDTAREV, GOA* inab.
A grounding device with a blocking arrangement*
Xlek.i. tepl.
tIaw 6 na.IW D 162. (MM 1622)
1. Nadallnik Shavehankorzkogo uchnatka
enerpmabshmiya, (for
Orabovetakiy). 2. Tekbuichaskiy otdel
Sherchemkovskogo uchastka
energoshabiheniya (for Cbebotarer)*
Mectric railroads-Wires and wirin )
(Electric railroads-Safety measureal

EP '(010tRWIFG0~ AFFTC/,IMvD.' '.SD-
-W)/FS(v)-2/BDS/ES(v) 3/
AP"
-Pd-4/?e-4/Fg-4/Pi-4/Fo-4/Pq-4- TT/Mi
AX-::,'SS~0,':,' NR: AR,-1002032 S/0269/6q,/000,/003/0003/00.0~P,
SOURCE RZh. Astrononiya. Otdelinyy vypusk. Abs. 5.31-112
jjjI
TI=-: Preliminary orbital e1 Is\81 the cabin of the first
_2~co ship (1960 e3)
ICITED SOURCS: Byul. optich. nablyaderiya iskussty. sputnikov
Zemli, no. 27,
19
TOM TAGS: satell t!a-orbital' elemani'S
T.WNSIATIO.N: 7ne, authors,Dresch a smnary of th emean equatorial
elenents of the
th
orbit o:C th6 cabin of t e first Soviet ,axtce ship as well as their
(1960 F-3)
tions Zrom 13 June to 27 S ep t C-'-..b e r1961. The Rements were
do'
daily vari vermined
on 'Une basis of 563 visual and prelim inary photographic
observations by Soviet and
foroign stations. Six.Tlifiod formulas are given for transforming
mean into osotx-
lating elements and ways to compare theory and observations. Mare
is a biblio.
grkphy of 7 ite-as. N. Yakhontova
DATZ ADZ: .;De',aY63 SUB tCOM- Al =M:, 0.0
Card 1/1

L ~19.3~ "-3 EPA(b) INT(l) /FCC(x4) /FS(v)-2 /BDs/r.-s(v)
AFFTC/AFMr;C/ESD-3/SSD/
-ikC ! Pd-4/Pe-~4/Pi'4/Po-4/Pq-4 TT/-GW
ACCESS110'N INIII: AR3002033 �lo!69163100010051000910009
SOU.Tta RZh. Astronomiya.. OtdolInyy vypask..Ab3. 5.31.113
AUIMOR: Chabotarcy, G,,L.-,,Bakarova, Ye. X.
TITLE: Prcli:mi=7 orbital elements of t-he cabin of t1ho fourtz
Soviet artificial
earth f~atellite (1960 C-3)
CTITIED(SOUIRM: Byul. st. 6ptich. nablyudenlya isImsstv. sputnLkov
Zemli. no. 28F
196z, 11-13
TOPIC MOTS: artificial earth satellite, orbital element
uatorial orbital elements for the cabin
TRANSIATION: 'The authors give the mean e5,,
of th e fo Art:kf itd-.-from 5 Oc er to 27 December 1961 and.
Z_tcial satell _ -
their secular perturbations. These data were obtained by processing
about 3.000
observations made by 89 Soviet and foreip stationse N. Ya.
ak v AcQ: 3o:-,.ay63
Card 1/1
SUB COM Al
BNCL: 00

ACCESSION NR: AT4001202 S/2511/62/008/005/0324/0334
AUTHORS: Chebotarev, G. A.j Kirpichnikov, A. K.
TITLE: The nfluence of.lunar shape on the motion of artificial
lunar satellites
SOURCE: AN SS 'SR. Inst. teor. astron. Byulletenl# ve 8#,,no* 5.
1962, 324-334
TOPIC TAGS: triaxial ellipsoid, lunar rotational axis, lunar libra--
tion, fictitious artificial satellite, perturbing forces vectors
polar orbit# pericenter and apicenter, equatorial orbit, inertial
moment, mutational constant, gravitational constant. numerical
integration. lunar mass, dynamic ablateness. lunar satellite peri-6
.center, artificial lunar satellite pericenter. orbit eccentric
anomaly, orbit mean anomaly
ABSTRACT: In view of the premise that a launching of an artificial
moon satellite will enable us to improve our knowledge of the
figure and mass of the moon (A. A. Yakovkin, Luna, Ch. 1. Fiamatgiz,
1960), the author determines by numeiical integration the effect of
Card 1/2

ACCESSION NR: AT4001202
the figure of the rotating moon on the motion of a fictitious arti-
ficial moon satellite. In particular, the rate of secular displace-
ment of the pericenter of the satellite orbit is calculated. Four
variants of orbits are considered for the moon's satellite, namely
polar and equatorial orbits with small and large eccentricities.
The secular displacement of the line of apsides due to the figure
of,
the moon is calculated. The main results of the numerical integra-
it
tion are tabulated. Orig. art. has: 36 formulas and 10 tables.
ASSOCIATION: Inst. teor. astron. AN SSSR,(Inatitute of Theoretical
Astronomy AN SSSR)
SUBMITTED: 22Apr6l DATE ACQ: 2lNov63 ENCLt 00
SUB CODE: AS* GM NO RZr 80Vs 007 OTHBRe 004
card 2/2

CHEBOTAREV, G.A.; KIRPICHNINOV, S.N.
Stability of the motion of artificial lunar
satellites. Biul.-
IL-st.teor.astron. 8 no.6:,402404 162. MRA 15.8)
(Lunar probes)

S/035/62/000/012/004/064
AOO1/A1O1
AUTHOR: Chebotarev, G. A.
TITLE: On occasion of publication of the 100th issue of the Bulletin
of
the Institute of Theoretical Astronomy
PERIODICAL: Referativnyy zhurnal, Astronomiya i Geodeziya, no. 12,
1962, 6,
abstract 12A29 ("Byul. In-ta teor. astron. AN SSSR", i96~, v. 8,
no. 7, 457 - 458)
TEXT: The contents of studies published in the Bulletin, beginning
from
the first issue dated on July 15, 1924,are briefly described.
[Abstracter's note: Complete translation]
Card 1/1

:ACCESSION NR: AT4040744 S/2511/62/008/009/0641/0646
AUTHOR: Chebotarev, G. A.; Dozhkova, A. 1.
'TITLE: Stability of elliptical orbits in the sphere of influence
of Jupiter
;SOURCE: AN SSSR. Institut teoreticheskoy astronomil. Byulleten',
v. 8, no. P(102), 19620
~641-646
!TOPIC TAGS, astrophysics, astr9nomy, celestial mechanics,
Jupiter, planetary influence t
ssphere, satellite orbit
i ABSTRACT: In earlier studies (Byull. ITA, 7, 8(91) and 8, 2
(95)) the authors considered
the problem of the stability of circular orbits (with direct and
retrograde motion of a satel-
lite) in the sphere of influence of Jupiter. In this new study the
numerical integration method
was used to investigate the stability of elliptical orbits (e = 0.
5) with direct motion of a
"tellite. As in the earlier studies, the author considered the
motion of six fictitious
satellites of Jupiter, moving in orbits with specific parameters,
with the origin of coordinates
at the center of inertia of Jupiter. Since the radius of the
sphere of influence of Jupiter is
R = 0. 279 a. u., all the six satellites considered lay deep
within the sphere of influence of
Jupiter at the beginning of their motion. The motion of Jupiter is
considered unperturbed and
occurring in a plane. The motion of satellites I-IV Is unstable,
as in the case of circular
[Card