SCIENTIFIC ABSTRACT OSTOSLAVSKIY, L.V. - OSETOWSKA, E.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001238430005-5
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: January 3, 2017
• Document Release Date: June 21, 2000
• Sequence Number: 5
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

AUT11ORZ: T.A. SOV/147--,
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PHASE I BOOK F"LOITATION SCrV/403.3
SOV/11-M-118
Ostoslavskiy, I.V., and T.A. Gr=ondz
0 avyazi mezhdu pod"yamnoy siloy kryla i kharakterom techeniya v pogranichnm
sloye (Connection Between the Lifting Force of a Wing and the Nature of
Flow in the Boundary Layer) Moscow, Oborongiz, 1959. 51 P- (Series: Moscow.
Aviatsionnyy institut imeni Sergo Ordzhonikidze. Trudy, vyp. 1-18) 1,100 copier,
printed.
Sponsoring Agency- RSFSR. Ministerstvo vysshego I aredne6o spetidallnogo
obrazovaniya.
Ed.: I.L. Yanovskiy, Engineer; Ed. of Publishing House: A.A. 10irustaleva;
Tech. Ed.: V.P. Rozhin; Managing Ed.: A.S. Zaymwakaya, Engineer.
PURPOSE: This book Is intended for scientific workers and instructors at tech-
nical schools of higher learning.
COVERAGE: The book covers inventigation.0 of moteaU motion in the boandw7 layer
Card 1/3

Connection Between the Lifting Force (Cont.) SOV/4013
at the initial moment after the beginning Ofairculation. It includes some
plienamens of the formation of the lifting force . Results of experiments
confirming theoretical considerations are given. These experiments were iqade
with noncampressible fluids, but they may be extended to cover compressible
ccmditions. The authors thank Engineer N.V. Korolev, Engineer 1,.Ya. Vasillyev,
Engineer B.I. Kinlrov, and Docent A.S. Povitskiy. There are 6 references:
5 Soviet and 1 English.
TABLE OF COMUM:
1. General considerations 3
2. Transition of the unstable flow to stable flov in the boundary
Wer 15
3. Experimental investigation 32
4. Conclusions 40
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Connection Between the Lifting Force (Cont - ) SOV14013
Appendixes:
1. Some r viarks on e xperimental methods and precision of tests 42
2. Experimental values of b oundary Layer parameters 45
Bibliography 53
AVAIIABLE - Iibrary of Congress
AC/ren/gap
Card 3/3 7-29-60

PHASE I BOOK EXP,,uiTAT1JN ' Ov / 1~1 i --, C
Ostoslavskly, Ivan Vasil'yevich, and Irina Vlktorovna Strazheva
0 formirovanti kontura upravlenlya samoletom (Forming Aircraft
Control Outline) Moscow, Oborongiz 1960. 97 p. Errata slip
inserted. 3,150 copies printed. ~Serles: Moscow. Aviatsionnyy
1natitut Imeni Sergo Ordzhonikidze. Trudy, vyp. 1214)
Sponsoring Agency: Ministerstvo vysshego I srednego Epetslal'nogo
obrazovanlya RSFSR and Moskovskly ordena Lenina Aviatsionnyy
Institut Imeni Sergo Ordzhonikidze.
Ed.: I. L. '-'anovskiy, Engineer; Ed. of Publishing House:
M. S. Anikina; Tech. Ed.: V. P. Rozhin; Managing Ed.:
A. S. Zaymovskaya, Engineer.
PURPOSE: The book Is Intended for a1rcra,"t Industry personnel. it
may also be used by Instructors and students In technIcal senools
of higher education.
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Forming Aircraft Control Outline ISOV/5130
COVERAGE: The book describes the general case ()f lonF;Itudinnl and
lateral maneuverability of modern aircraft, equipped with auto-
matic devices. Air compressibility Is taken Into account. The
problem is treated linearly ,with the help of simple methods of
the theory of aircraft regulation. Approximate graphic and an-
alytical methods for determining the center of gra%Ity and the
transmission ratios of the automatic systems are determined. A
method of Improving the maneuverability characteristics and the
controllability of aircraft at high altitude through the use of
automatic stabilizers is discussed. The iuthors ttank A. M. Letov
and N. A. Kheyfets, Doctors of Technical Sciences, and
I. L. Goloborod:ko and A. Ya. Vasil'yev, Engineers. There are
4 references, all Soviet.
TABLE OF CONTENTS:
Foreword
Conventional Signs 5
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A"022014 BOOK MLPWTTATION S/
Ostoelavokly., Ivan Vasillyevichl Strazhevap Irina ViKorevna
night dyna-micel trajectories of flying apparatuses (Dinsimika poletetl trayektorii
letstellny*kh apparatoy) Moscow, Oborongiz, 1963. 430 P. illus., bitillo,
Errata alip inverted* 11,000 copies printed. (Textbook for aviation Tuses
and departments) Publishing house editors M. F. Bogomoloval Technical editors
V. L Oreshkina; RevJewerat Profereor Kurehev,, N. V., Professor Tkaebonko, Ya.
Ye.; Editors Docent Kotlyar, Ta. Y.; Chief editors Engineer Krasillnikov, S. D*
TOPIC TAGS: FliEht dynamics, flight trtjectory,, airplane,, guided missile, ballie-'~
tic rocket, rocked plane,, equation of notion,, problem of Mayor,, time standard
atmosphere, dynamic coiling, maneuvering, flight range,, effective radius
FJRPOSE AND COVERAGEt This book Is a textbook for students at aviation vuzee and
conforms to programs In flight dynamics. It can be used olso by engineers con-
cerned with the design of flyIng apparatuses. In this book,, methods of computing
the flight trajectories of different flying apparatuses - ai"lanes, Saided, als-
eiles,, ballistic rockets,, and rocket planes - a" describede Methods of optla1-
sing flight trajectoriop based on the apnlication of irarlational calculus are
Cord

AH4022314
anal7zed. Brief information in presented concerning the application of mathematic
apparatu3 to problems of flight dynamics. Problems of the maneuverability and
stability of flying apraratueee are to be analysed in the eeowg book to this
general subject* The authors thank Professor@ U. Too Tkacbenkv &W No V. tur-
shey and Docent ra. M, Rotlyar,
TABLE OF CaM=s
Foreword 3
Introduction - - 5
Ch. 1. Equationa of motion of a flying apparatus
1. Equations of motion of a body of variable composition 15
2. External forces acting on a flying apparatus. Cowdinate eyettma used for
solving problems of night dynamics - - 25
3. Equations of motion of a flying apparatus as a material point of variable
Maas - - 35
4. Equations of notion of a flying apparatus in a velocity coordinate system in
particular oases@ Squations of motion in terrestrial and In polar (inertial)
coordinate votow
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AW22014
Ch, 11. Mathematical bases for computing the flight trajectories of flying
apparatuses
1. General remarke concerning the integration of the equations of motion of a
flying apparatus - - 55
2. Numerical integration of the equations of motion of a flying apparatus 58
3. Integration of the equations of notion of a flying apparatus with the aid
of computers - - 66
4o variational problems of flight dynamics. Basic propositions of variational
calculus - - 69
5. Types of variational problems encountered in dynamics 78
6. Examples of the application of variational methods to solution of flight-dy-
nOniC3 problems. Uayer's problem - - 86
Oh. 111. 1Uw data for computing the trajectories of flying apparatuses
1. Parameters of the atmosphere. The time standard atmosphere (VSA-60) 101
2, Aorodynamic forces acting on a flying apparatus - - 103
3. Kinetic heating of the surface of a flyIng apparatus - - 114
4. Characteristics of engines used on flying apparatuses - - 122
Ch, IV* Stable motion of a flying apparatus@ EquMbrium fllght conditiaw
1. Rectilinear stable action of an airplane@ The tbrast notbod ckf So Too
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AN4022014
Zhukovskiy 134
2. Method of powers. Other rwthods of aerodynamic computation IA-7
3. Designing a flying apparatus in a homogeneous medium - - 160
4. Curvilinear stable motion In the horizontal plane. Banking of the flying
apparatus - - 163
Cho V. Nonatable motion of a flying apparatus In the vertical plane
1. Motion along rectilinear tra-Inries witttout banking and slipping. Pulling
cut of a dive. Climbing - - 1~t,,
2. Cptia= flight trajectory of a flying apparatus in the general case - - 182
3. Optimum take-off trajectory of an airplane with ram-jet eneinee - - 191
4, Computing the optimum take-off trajectory of an airplane with ram.-jet engines.'
Nuntrical. example - - 199
5. Optimum rocket take-off trajectory (horizontal-fl4;bt rangs unlimited) - -214
6o Sinpleat problem of Intercepting an aerial target saving In the vartle4l, planar
- - 216
7* Dynamic calling of a flying apparatus 2.11
Ch. V1. Nonstable notion of a flying apparatus In the vertical plane
soace of additional kinematic relationships
Ln the pro-
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A314022014
1. Uethcd of guidance by the pursuit curve 232
2. kethod of guidance by a beam (method of three pointe) 241
3. Lineari7ation of equations of guidance by the method of three points 248
4. Uethod of parallel approach. Other guidance methods - - 255
5. Crapho-analytic method of computinr, the trajectories for rocket gu!Ldance by
means of succee3lve approximation." - - 263
Ch, VIL Nonstable motion of a flying arrar&tus In the horisontal plane.
Concept or a spatial maneuver
1. Nonatable banking of a fWng apparstur 276
2. Problem of overtaking a moving target with a flying apparatus in the hori-
sontal pl4ne - - 283
3. Kinematic bases of guidance of & flying apparatus In the horizontal plane -
4- The ccmbat climbing turn, Other spatial maneuvers - - 294 - 287
Ch, VIM Nonstable motion of a flying apparstAis in the vertical plane with speeds
elope to circult speed I
1. Computing the glide portion of the flight trajectory of a baUlstle rocket
.0 3W
2& Computing ths ponr portion of t~,e trajectory of a ballistic rockoit 317
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3e Selecting the number of stages of a multistage rocket - - 326
4, Computing the range of a three-stage balliatic rocket* Numerleal example -
5. Computing the night trajectory of a rocket plans - - 338 - 331
6. The concept of computing the Initial portions of the trajectories of space
ships - - 346
Ch. IX. Computing the range of an airplane (quanietable motion)
1. Basic definitions. Per-kilometer and hously fuel consumption - - 351
2. Computing the rangre of an airplane with ram-jet engines (VRD) - -354
3. Computing the range of an airplane with propeller engime - - 372:
4. Effective radius of an airplane. Means of increasing Ithe range s.nd the effso-
t1ve radius - - 373
5. Computing range in the presence of wind 384
Ch* X. Starting and landing characteristics of a flying apparatus
1. C=Iutine- the starting of baUlstic rockets 388
2. Co.%ruting the starting of winged rockets 391
3. Starting an airplane 403
4. Computing the take-off distance of an airplane - 9A
5. Computing the landing distance, of an airplang "I
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AW22OU
Appendix. The time otandard atmosphere (VU4
Literature
MB CMBI A rp Alp WENITMe MuS63
D= ACQs 5H&r64
CwJ 7ft

L 168gh-66 EWT(d)1FSS-21EB0(k)-2 GSIM
ACC NR: AT6035713 FOURCE CODE: U11/00/65100/00/0302/0307
AUTHOR: Pstoslavskiy, 1. V (Professor, Doctor of technical sciences)
ORG: None
TITLE: On the expediency of stabilizing the pitch angle when flying in a turbulent
atmosphere
SOURCE: lasledovaniya po, dinamike poleta. (Research on flight dynnrnicis), no. 1.
MoBcowp lzd-vo MaBbinostroyenlye,, 1965,, 302-307
TOPIC TAGS: aerodynamic pitch, aircraft autopilot, motion stability, aerodynamic
stability, atmospheric turbulence q 10
AWMACT: The article deals with the role of the aut9211 channel which stabilizes the
pitch angle during flight in a turbulent atmosphere. Horizontal flight Is assumed to be the
programmed flight mode. The following simplifying assumptions are postulated In the
solution of the problem: 1) the flight speed of the aircraft is considerably less than the first
comic speed, and the effect of the Earth's curvature on the aircraft flight characteristics
are diBregarded; 2) the diurnal rotation of the Earth Is not taken ipto account; 3) changes in
density,, temperature, and pressure of the environmental air In the process of turbulent
Card 1/2 UDC 629.19.04.005

L 16894-M
ACC NR: AT6003578
motion are disregarded; 4) the aerodynamic forces acting on the aircraft are determined
in accordance with the steady-state hypothesis (cxcept~ for the downwash at the bill); 5) the
angle-of-attack is small ED that the propulsive force component normal to the flight tra-
jectory is disregarded; 6) the effect of elevatcr deviation on the lift of the aircraft to dis-
regarded; 7) the autopilot Is Ideal; 8) the problem is solved in a linear formulation. It to
shown that, provided It Is possible to ensure satisfactory transient process quality and
other indices of controllability and maneuverability without pitch angle BtabIlization, the
use of such stabilization to improve flight conditions In turbulence is not advisable. Orig.
art. hasi 3 figures and 12 formulas.
SUB CODE: 01 /SUBM DATE: 02Aug65
Of/
Card 2/2--t4

L .16895-66 W(d)IFSS-21EW(I)IEWP(m)IEEO(k)-21&IA(d) 03/ow/BC
ACC NR: AT6003579 SOURCE CODE: UR/00DO/65/000/000/008/0337
AUTHOR: . 0stoslovskly, 1. V. (Professor, Dnetor of technical sciences) -..�Lrav,hevn. 1. V.
ORG: None
TITLE: The design ofan oil-board stabilization symtem or a pilotless flying craft
SOURCE: Issledovanlya po dinamike polets (Research on flIght & dynamics), vio. 1.
Moscow, lzd-vo Mashinostroyenlye, 1965,, 308-337
TOPIC TAGS: aircraft automatic pilot, stabilizer, motion stability, aercidynamic
stability
ABSTRACT: The authors consider the purposes,, requirements, design, and configuration
of an on-board stabilization feedback system for a pilotless flying craft. The transmission
funcition for such a system is derived and analyzed. Primary attention is given to the
formation of an on-board stabilization system which will provide satisfactory 'transmission
of control signals over the entire range of required frequencies with a trinetent process of
satisfactory quality, regardless of the problem of a reduction of the harnifti effect of Inter-
fereLce. The craft is considered a second-order element (oscillatory or apeflodic), so
that if the real automatic pilot, Is replaced by an ideal devicep the amplitude-firequency
Card 1/2 UDC 629.19.04. 00f,

L 16695-66
ACC NR: AT6DD3579
19
characteristics of the on-board stabilization system will be of a quite definite form. If the
maximum control frequency is small then the required eigenfrequency of the craft (an air-
craft, for example) with the autopilot will also be smallo and the problera can to solved
without the introduction of any correcting clements. Basic expressions and tronsmi8sion
functions for a case of longitudinal motion by the craft are derived, together with similar
equations1for lateral or translational motion. On the basis of the mathematiciJ model,
the authors describe an on-board stabilization system for a pilotless flying craft, assuming
an Ideal device in place of the autopilot, and the effect of rudder movement on the genera-
tion of aerodynamic forces acting on the vehicle Is disregarded. The paper coricludes with
an estimation of the errors due to the substitution of the Ideal autopilot for the real. Orig.
aA W: 7 figures and 136 formulas.
SUB CODE: 01 SUBM DATE: 02Aug65 ORIG REF: 005
Card 2/2shf

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BE"."-'IC, Dr Z., ana of -,~o -'~tampar
Scr.ool ( Skola :;aroa:-.or7 Zarav. --a an,; -..%r;
Ilublic Health jtr,-.io.. ~ ~-om in
"Infec,io-,is of
Bolgrade, Vo 9 6 3
Ab~itract: ~Tlut-o--s' modirie-!7 t,-, o~
in;'octio,,.-i in tno vac.~.it.i o.' tho :, -o j,*'
Koncanica LiStrt~.' 7,,)70 thar. a ,-,Lr ani % .1il,illf. T~,, o i. o t o
detei-mine whetner ~he ear-y of sufferers
prevent the further ozreau of ne ;.Jouase, but tno iooatior, of
Tationts did not c'-eck tnu oPi,~czmlc. .'he leni-th of the o;,iJar.-,'c
was probably due to the t-rj-,c.,3 of oc-tir-ments (onn vilarn-3 -`or.~,
'r,oth :-,ides of P- road, ano-,ner huadle-J -Jr the imido: of a wo~do,
arothor on nei;-hborinE; hills, -,' ' -.,-4.*h a zinj--e cc7.-cn a.emo;-,tiry
school) ara h:,-,.-ienic ccn-,i*.Ior..,j . :Iiotoctu.,~ rrj z;Cw~iI,-e
dispossal systems, but ear'.y hoopit.%.ization may navo -,~L-Jod a
1717part. 'No tables, one b-raph, four YuCoslav refe-ences
28

DSTXAW730, J.
Parinand's oculo-glandular syndrome. Cask. opht. 10 no.6081-387
Do c 54.
1. Z 11. ocni kliniky Karlovy university v Prare - prednosta
prof. Dr. Jaromir Kurz
(M.MVBS. OCUIOMWOR. paralysis
Parinaud's synd.)

Ahl)RFYEV , A. 0 irvardi I ':'3.~,j Y ) V. . gvardll ~,)j i tan
Muscles of :;toed. Vo~-n.vuat. 43 no.1106-38 1; 163.(KIRA 16:12)

OSTRUZ, L., inz.
Support for the nationa-l economy in the Wroclaw Voivodeship. Frzog!
techn 84 no.16:5 21 Ap 163.
1. Przewodziczacy Oddzialu Stowarzyazenia Elektrykaw Polskich,
wroAlaw.
.0-~ . "

OSTRAUSKI-ENE, S.
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DP AIC G --- L I :E:
KA71LME,
Th- T- 7 ,-r tr(-.1. Svp ' k . apgaug.
r)t,
1. Kwiro Va'lrt. r -;tar- (rcll-.tor!us - -,rof.
;.-P Kwirn klit i7 - llf-rr ~ne

OSTRATAP TU.
Incubator for tomatoes. !Un.tokh. 7 no.5t6O ~V 163. OURA 16:6)
(Growth promoting substances) (Tomatoes) (Ethylene)

,i:,ILISSKATA. 7e.A.; OSTRAYA, S.S. .
il-nckhends and nimpleG in Wants. 7es~. der=. i ven. 3"' -0-2:
B2-83 mr-Ap 159. (141A 11-:7)
1. 12 -(02hno-venero loe, icheskogo dispannera 14oakvy.
(SYIN-DISMSES)

KRACMER, M.; OSTRCIL, F.
Pertroeharteric fracturee (incidence and result6 of conser-m-
tive treatment). Rozhl. chir. 42 no.7:4,80-483 Jl 163.
1. Vyzku=y ustav traumatologlcky v Brne, reditel prof. dr.
V1. Novak, DrSc.
(MORAL NECK FRACTURES)
(FRAMM FRATION)
(AGED)

MASTNY, V.; OSTRCIL, F~
Reatoration of joint mobdlity after injury. Rozhl. chir. 42
no.7:454-458 J-1 163,
1. V3rzkt=y uatav tratmtologicky v Brne, reditel prof. dr.
V1. Novak, DrSc.
(FRACTURES) (JOINTS) (RERABILITATION)
(DISABILITY EVALUATION)

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-T,
)OS
=R/Geography - Arctic explorations
rArd 2A t Pub. 86 - 1138
Authors I Ostrekin., HOYE*
MID I Most recent researches in the Central kretics
Periodical i Pr1roda 43/12.s 3-12.9 Dec .1954
Abstract I A historical accowAt Is given of aggaorations in the Arctic regions#
culuinating in the opening-up of shipping passages* The methods of
eiploration are explained. Theme methods enabled the scientists to
set up stations and conect data on the earthle napetisaj, air temper-
aturess direction and speed of ice novammt., and the depth of the
oceane The last mentioned data being incorporated into vzy3 sa shown*
MajAj i1lustratiow,
Institution 3
Subvittod

OSTR M N, H.Te.. geroy Sovetskogo Soyuza.
"etic anomaly in the central Arctic. Priroda 45 no.7:127-128 JI 156.
(Arctic regions-Magnetism, Terreetrial) 4KIRA 9-9)

84589
1j/16q/6o/0OO/O01)/0,')7/C)0 -
3, Flo 0 A005/A001
Trarmlatlon Irrin: 101crativriyy zhtly-11111, Ook2flzlka, V)60, No, 1), p~ "U4. # 1104"
AUMOR Ostrekin, M,ye,
1__~
TITLE, Some P eliminarl Concluslons on the G,:ographic Distribution of
Dailyvmu~M,etlc Disturbances In the South Pole Real n According to
the 0b,-rrv-a-t1TTr-Results Obtained in 1958 ~ V-0
PERIODICAL. Inform. byul. Sov. antarkt. ekspc-dit-sil, No 6, pp. 32-54
TEXT- The geographic distribution of magne~lc d1slurbances Is analyzed on
the basis of the data from the antarctic stations. Tile Investigations showed a
well expressed diurnal course of the magnetic activity at these stations The
distribution of the Instants of maximum magnetic disturbance gives rise the as-
sumption that the helix scheme obtained from the data for the aretic region re-
mains, obviously, valid In principle also for the South Pole region. It is as-
sumed that a secondary zone of enhanced recurrence and Intensity of the polar
lights exists In both the circtunpolar Antarctic and the Arctic regions
Kh.D Kanonldll
Translator's note: This Is the full translation of t.he orginal Russian abstrart.
Card 1/1

OSTRIMIN, M,Ye., kRnd.,veograf.nauk
Scientific results of the Yburth GontInental Irpedition. Infort.
blul. Sov. fntark. eksp. no-2115-7 160. (HIRA 13:10)
1. Arktichookly i antarkticheekly nauchno-iseledovatellakiy Ingtitut.
(Az)tarctic regions-Rusdan exploration)

.1
05THEKIN, M.Ye., kjLnd.VE--otva-f.nau1,
J I
Sixth Antarctic Eypodltion. Inform. biul. Sob. antark. n,).2-1-.
8-10 '61. (MI i A 14: 5)
1. ArIcticheskiy i &ntarkticheskiy nauchno-isoledovatelli3kiy institilt,
(Ant-arctic regions-Russian exploration)

LEDEDEV, Vladitir LIvovich, kand. geogr. nauk;-Qff_RI&B,-kUIhaiI-
Yezellyanovich, kand. geogr. nank, red.; TOISTBOV, Yevgerdy
-Tv-i-no-y-f-ch-, -Fa-R.--geogr. nauk, red. ; UPLINSKATA, L. G. , red.
KOTIZAKOVA, 0.1., tekbn. red.
[Transactions of the Soviet Antarctic ExpeditionlTrut Sovot-
skoy antarkticheskxo ekspeditsii]Leningrad, lzd-vo I'llorskoi
transport." Vol.16.fThird continental expedition, 1957-1959;
general &3cription and scientific remltg)Tretlia kontinen-
talInsia ekspeditsila, 1957-1959 gg; obshchee opiBnnie I
nauchrWe rezul'taty. Pod red. M.E.Oatrekins i E.I.Tolstiko-
va. 1962. 327 p. (MDIA 15:~,)
1. SovetBksWa antarkticheskaya ekspeditsiye, 1955-. 2. Eachal'-
nik Tratlyey kontinentallnoy ekspediteii, 11~55- (for Tolstikov).
(Antarctic regions--Geopt7sical resoarch)

L 0303~-67 F-rl (1) T4
AZC Nil, '77001680 SOURCE CODE: UR/3174/65/000/055/0005/0011
-,r. OR :Ostre,,,in, Ye . (Head of the 10th aca3onal Antarctic expedition)
L73 : Arc c ana Antarctic Scientific Re3earch In3titute (Arkticheakiy i
antarA-~1C.-43Ki.y nauchno-issledovatel'skiy in3titut)
Resul' the
I ~s of the work of tenth seasonal Antarctic expedition
5 G15 -, 0 H :Sovet5kaya antarkticheskaya okspeditsiya, 1955-. Informatsionnyy byullaten',
no. 55, 1965, 5-11
70?:C 7AGS: antarctic climate, son ice, oceanography
~-C, T F~'% C T :7~,v on.4ectives and results of the "I'enth )oviet Antarctic Eypodition are
given. All Lhe basic Objectives for the January-Mirch (1965) season were
Mct: 1) SOV01ILY-SiX oceanographic scatibns were occupied between Mirnyy and
Novolazarevskaya along profiles which previously had never been studied, or
only very litcle. 2) Detailed observations of ice and icebergs were Mide
wiLh pi',oLorecording of the radar screen. 3) Precise recording of Lhe rhore
was accomplished along about 500 miles of poorly investigated coast between
"~Ur- y
, n y and Novolazarevskaya. 4) Depth soundings were made for a distance of
abouc 7,000 miles between Mirnyy and Novo lazarevskaya with quite frequent
tie-in WiLh ASLronomical determinations. 5) Six oceanographic stations were
occupied in the zone of the Antarctic convergence. 6) Two acientific treks
were made for a distance up to 100 Ian from Mirnyy for geodetic determinations
and determination of thickness of the ice cover by the electromagnetic method.
-Card

L 08085-67
ACC NR.
7) C;errman specialists determined precise gravity values at Mirnyy and Molo-
dezhnaya and reduced them to the reference point at Potsdam. 8) The attached
American biologist collected mosses and lichens at Mirnyy, Holodezhnaya and
Novolazarevskaya. 9) Vostok was fully supplied by air. 10) A round-trip
flight with japanese scientists was made from Siowa and*back. 11) Personnel
at all stations were replaced and all stations were supplied; the "Ob"' brought
3,700 tons of cargo and the "Estoniya" about 200 tons. In addition, much
construction work was done at Molodezhnaya and much repair work at Mirnyy.
A special gravimetric observatory ~!as built for Germ-in scientists at Holo-
6ezhnaya.,:_Co_ntin_u-ous shipboard meteorological observations were maa-S.Iie-
anQ weather conditions were good during the field season. Orig. art. has:
1 figure. IJPRS: 37,397)
SUB CODE: 04, 08 / SUBM DATE: O3Jul65
c0, J

OSTREKIN, M.Ye.
Yishing in Antarctica. Inform. biul. Say. &ntark. eksp. no.39:
"-45 163. (MIRA 16t 6)
(Antarctic regions- Fishing)

OSTRE-KIN, M.1e.
"Marked" Iceberg. Inform. biul. Say. antark. eksp. no.1-18:47-4',
10. (MIRA lt,:7)
(Lazarey Station region, Antarctica-Iceberp)

1.
IDIALIFA-704 Ch.M.1 Q'Ja2'.5.KlYg
ThnnowAlyUc 6DtandmtIon of thD can~ont of aidorito
(zasmtdi- ciaorite) in farrucinow ourbumton. lmv*Ali
Amrb,`,"14 Ser.raole,-CoM.rxwk no.2s63-67 164.
(1,L- RA is Ill.)

ANDRETEV, G.Ya., kand.tekhn.nauk; DAVIDBKO, N.P., inzh.; MALITSKIT,
I.F., inzh.; WTRENKO,,B.S.k inzh.; SHATIKO, I.I., inzh.
Using induction heating In setting and dismantling wheel pairs.
Mashinoetroenie no.6s67-71 N-D 162. (MIRA 16:2)
1. Kharlkovskiy gomyy inatitut.
(Induction heating) (Car wheels)

AVDONIN, A.K., tnzh.; Or)'TTTNYO, V.S., lnzh.
Device for reglete.-Ing tbe 1~
rectifiers &nd prcto.,ctors. Flek'.rG*,Akhnik& 36 no."U.4-46 .71 '-,c.
'MIRA '1-2,-'

Do- C,rt; ti crd I'l-, A rj ti cn o I' the for-E.,
for rrzui,~rel drwwi tit- in a i ilgrim mill. F'roi z-v. trub nc,. 10: 7-14 63.
O,a""A 17: lo)

--OSTR&NKO, V.Yq. ; FLINICHEV. I.a.. rodaktor.
[Skilled worker in the drill and casing pipe section; textb-ok
for practical P~nd technical colirses ard schnolg for skilled
workeraj Master otdela burtl'nykh I oboadnykh trub; uchabnik
d1i& proizvod9tvenno-teirhn.k-ur9ov i elikol vaeterov. KhAr'kov,
Gos. nauchno-tekhn.izd-vo 111t-rv po chernoi i tsvetnoi metallur-
gli, 1953. 179 p. (MLR-A 7:))
(Petroleum-Well boring) (Boring machinery)

7. Ya. ostr(~n~o, iri.-alir 1~aril'i-,-, 11, i~i- ~n r
rizdat, P
Df,scri ,lIq 'xo,~ rv),!,,rn 11 1, 1 !7. Ir I I ;, i , -s 1 e I J, 1)
w r, n I r, ca I i i i' r,(, ne tt,. n -
-a in rul,- )r ~~e roct-,:~,; ~o! n-

s,?' ~.i ii - r ni-s. j
Che br) ,k i,- t n I --Ac I ir t,),t r w
o-arses aiii re-- i
12

ACCESSION NRt ARbO1046 S/0137/63/ODO/012/DO35/DO35
SOURCEt RZho listallurgiya, Lbs. 12D21L
ALITHORt Q~.trenkop V, Ye.; Dferov, V. M.1 Geyko, 1. K.; Pechennikova, 1. Sol
Lagutina, R. Vol Kirvalidze, No So
TITM Hot rolling of pipes from EP38, ZP39, and E1993 steels
CITEDSOURCEi Sb. Proiz-vo trub. M., Yetallurgizdat, vy*p. 9, 1963, 5-12
TOPIC TAGSi Steel pipe hot rolling, pipe steel composition, steel pipe rolling
TRANSLATIONi Chemical compositions of the indicated ateela to be used in pro-
duction and the mechanical properties of the tube blanka are given. The mech-
anical properties of these steels are examined in detailo The mechanical pro-
pertisa of the pipes obtained are indicated, and reconnendationa designed to im-
prove the quality of the pipes are given for the procedure of their hot rolling.
DATE ACQt 09Jan64 SUB ODDEs n ENCLs 00
Card 1/1-

- . ~.. %'.Y'L. I , - -1. . ! -1. . 1, ~ " ; ~ - I - . I "'. . . , I ;- - - ; A . I I . . . . iI
- - J .",
4 ., ,_, - ,, P, 9" I - . , - -.. .
-, - -'- - . , - . -i :. - i. - - - - . -
. . - - . . . . I I .. - :
I
,,I, - " ; - . - ~ I I -

ACCESSION NR: AT4007048 S/2598/63/000/010/0254/0261
AUTHOR: Ostrenko, V. Ya.; Sagoyovienskaya, N. V.; Bobrikov, L. D.; Aklmova, Ye.
P.; Usov, i_.K.; L. N.; li'vovskaya, L. A.
TITLE: Development of a production process for AT-3 titanium alloy tubes
SOURCE: AN SSSR. Institut metallurgil. Titan I yego splavy*, no. 10, 1963.
Issledovanlya titanovy*kh splavov, 254-261
TOPIC TAGS: titanium alloy, AT-3 titanium alloy, AT-3 alloy tube, tube rolling,
hot rolling, cold rolling, AT-3 titanium alloy property, titanium aluminum chrom-
ium alloy, Iron containing alloy, silicon containing alloy, boron containing alloy
ABSTRACT: The effect of thermal treatment on the mechanical properties of AT-3
alloy and parameters affecting the cold and hot rolling of tubes of this alloy
were investigated in the laboratories of the Ukrainskiy nauchno-issiedovatellskly
trubny*y Institut (Ukrainian Scientific-Research Institute for Tubes) and the
Nikopol'skly yuzhnotrubny*y zavod (Southern Tube Plant. Nikopol). At temperatures
of 800-900C the mechanical properties and hardness of AT-3 were markedly altered
by hardening In water but essentially unchanged by cooling In air or In a klin.
This effect Is explained by the fixation of the Intermediate a + 0 structure dur-
Ing hardening In water. These alloys daimonstrated high ductility In a w1de range
Coid 1/2

ACCESSION NR: AT4007048
of rolling temperatures (1975-1125C). A maximum deformation of 55% can be attain-
ed by cold rolling of such tubes, while hot rolling of these tubes proceeds normal-
ly. The problems Involved are sticking of the metal to the rolling device and the
formation of a gas-saturated film on the hot rolled tube. These problems have been
solved by additional mechanical treatment~Wch as etching. coating with an oxide
film.and lubrication with a mixture of castor oil and talc. Some of these recom-
mended procedures are discussed. Orig. art. has: 6 figures and 3 tables.
ASSOCIATION: IsIoUtut matanurgLi AN SSSR (Metallurgical Instl tute#AN MR)
SUP14ITTED: 00 DATE ACQ: 27Dec63 ENCL: 00
SUB CODE: MA, ML NO REF SOV: 000 OTHER: 000
Card 2/2

ACCESSION NR: AT4007059 8/2598/63/000/010/0357/0361
AUTHOR: Ostrenko, V. Ya.; Akimova, Ye. P.; II'vovskaya, L. A.
TITLE: Investigation of AT-4 titanium alloy suitability as tube material
SOURCE: AN SSSR. Inatitut metallurgii. Titan i yego splavy*, no. 10, 1963.
Issledovaniya titanovy*kh splavov, 357-361
TOPIC TAGS: titanium alloy, AT-4 titanium alloy, AT-4 alloy tube, AT-4 alloy hot
ductility, titanium alloy tilbe, tube rolling
ABSTRACT: The six-component titanium-base alloy AT-4, developed previously for
sheet-rolling and forging, has been investigated for suitability for seamless tube manu.-
facture by hot rolling. The chemical composition of AT-4 is 3.6-5. 0% A 1, 0. 4-0. 9% Cr,
0. 25-0. 60% Fe, 0. 25=0. 60% Si, 0. 01% B, and the rest titanium. Basically, aluminum is
an alpha stabilizer; and chromium, iron, and silicon are beta stabilizers. At room
temperature the alloy consists mainly of alpha-solid solution and a small amount of beta
phase. According to a practice adopted for testing of materials for tube manufacture,
the alloy AT-4 has been tested in hot twisting and piercing. Phase transformation and
response to heat treatment have also been studied. It has been found that the number of
Wet turns-to-failure increased sharply from 9 to 28 with an increase in temperature from
Card 1/2

ACCESSION NR: AT4007059
goo to loon; the number of turns increased further up to I 100C. and decreased beydild
that point. From twisting tests it has been concluded that plasticity of AT-4 is slightly
lower than that of pure titanium, but higher than that of carbon steel. Further, hot rolling
of AT-4 alloy seamless tubes to possible in a temperature interval from 1000 to 1200C.
In piercing tests, conclusions on plasticity have been made from the surface appearance of
test barrels and from loads transmitted to the press. It is concluded that piercing can be
normally performed at 1050-120OC; at lower temperatures defects develop In the barrels;
i at higher temperatures clamping conditions of barrels got worse. Titanium barrels were
of higher quality th= similarly produced carbon steel barrels. It has been established
that AT-4 responds to beat treatment. Orig. art. has: 6 figures.
ASSOCIATION: Institut Metallurgii AN SSSR (Metallurgical Institute AN SSSR)
SUBMITTED: 00 DATE ACQ: 27Dec63 ENCL- 00
M CODE: MM NO REF SOV: 000 (MER: 000
i Cord 2/2

ACCESSION NR: Ap4o41538 S/Ol 37/64/000/004/D04 1/D()4 2
SOURCE: Ref. zh. Metallurglya, Abe. 4D248
AUTITOR: Ostrenko,, V. Ya.; Yuferov, V. M.; Geyko, 1. K.
TITLE: Mastering production of pipea from atell 12Kh6S2M
CITED SOURCE: Sb. Proiz-vo trub. Vy*p. 11. M., Metallurgizdat. 1963, 7-9
TOPIC TAGS: pipe, pipe production, rolling, heat trentment/12Kh6SPM ntpol
TRANSLATION: In the development of production technolor_y of pipes from steel
1M652-M there was investigated metal of pdpe billets of composition (%):
C, 0.12; SA., 1.53; Cr, 5.12; Pil, 0.38; Mo, 0.70; Nb, 0.25; Ni, 0.25; 3, 0-014;
P, 0.015. Bi-1let3 had diameter 85 millimeters and length 900-1000 millimeters.
Experiments for piercing were conducted on the laboratory piercing mil-l of the
Ukrainian Scientific Research Institute of Pipes. Rolle of the mill had :in
pressing a diameter of 140 millimeters and angle of entrance and output cones of
3*301. There were rolled teat pieces of diameter 35 millimeters and length 90
Card 1/3

ACCESSION NR: AR4041538
millimeters. For comparison there were pierced also test pieces of Steel 10.
During rolling they measured the load on the motor of the piercing mill and
pressure of metal on the roller; temperature of heating was determined by a control
piece with a thermocouple. During pressing in the 16% press, a cavity wan uncovered
at all rolling temperatures; with increase of temperature dimensions of the
cavity decreased, which corresponded to results of twisting tests. During pressing,
of 10%, openings of the cavity were not observed. Procer0ing from given data,
the temperature of piercing was selected within 1220-1250'. Rolling of 1pipeo
was produced an automatic installation 140 with a roller-type piercing mill.
Before piercing, billets were heated in a Hoffmann kiln for 50-60 minutes. During
piercing, adjustment of the piercing mill wan the following: diameter of rollers
738 millimeters distance between rollers in narrowing: 76 millimetfira, between
3traightedges: 83 millimeters; diameter of mandrel: 68 millimeters; advancement
of blade of mandrel beyond narrowing: 37 millimeters; diameter of housing: 93
millimeters; thicknese of wall of housing: 1-1 millimeters; pressing before
blade of mandrel: 5.3%, calibration of rollers symmetric with angle of conicity:
3*30'. Load on mill motor 850-950 kilowatt. On automatic mill, housings were
rolled in gauge of 88 millimeters applying maxidreI5 70 mil-Umetera in diameter.
During the firat paue and 72 millimeter during the aecond paos. On the rolling
mill pipea were rolIed up to a diameter of 96 millinetere, after which they were
Card 2/3

ACCF!',51011 NR: AR1401#1538
calibratW to finished dimennion 89 x 8 millimeters and subjected to straightening.)
Investigation of branch connections cut from finished hot-rolled pipes showed o
that their metal had a marten3ite structure and waE) characterized by the following.
properties: Ob , 143 kg/cm2; 9,, , 123.5 kg/cm2; 8 , 6.5%, ak , 9.3 kg/cm2;
and hardneso 302 Intermediate heat treatments of pipes in the process of
cold rolling con5a-ted in annealing at a temperature of 760-760' which ennur"d
removal of work hardening, pre3ervation in the metal of the atructure of granular
perlite and reatoration of mechanical properties. On the basio of conducted
investigatione there was developed the technology of production and prepared.an
experimental lot of boiler tubes of brand l2Xh6S2_H ateel.,
SUB CODE: IE, HN ENCL: 00
Card 3/3

bEC11 I JIGH-POlhO , A. I.; Cj,,3TRi.NK( , V - Y& -
W&-,r 5 (-, f & I I t (~fr.A T, I n,! p I I,, m I I I ~, .1-ju t . I ~, -, r n,- r A . pr nrL . ri ~ - , ;
(MIRA 11"i '
40-41 Mr-Ap It-).' .

0
ACCESSION NR: AP4019481 S/0133/64/000/003/0258/0263
AUTHORt Ostrenko, V. Ya.; Yufarovo V. M.; Geyko, 1. K.; Ty*r, V. P.;
Oslon, No At; Chererinskaya, R. I.; Vil'yams, 0. S.; Lagutina, R% V.
TITLEt Manufacture of tubes from now ferritic martensitic heat
resistant stools
SOURCE: Stal', no. 3. 1964. 258-263
TOPIC TAGS: heat resistant steel. steel tube. ferritic martensitic
steel. tube rolling
ABSTRACT: The authors report on techniques developed in recent yeais
by the Ukrainskiy n.-i. trubny*y institut (Ukrainian Tube Research
Institute) in cooperation with tube factories in Pervoural'sk and
Nikopol for hot rolling and heat treatingof tubes made from 9 new types
of steel, all of which contain 10-14% Cr and addition& of V. Mo, Nb,
and W. The AC temperature was in the range of 810-830C; ferrite
grain growth was noted above 1100C; piercing temperatures varied from.
1090 to 1200C. Ductility at high temperatures was found to depend on
the content of free ferrite. and piercing of tube*billets presented no
Card I / 2

ACCESSION NRz AP4019481
difficulties at a content of 50Z. At 15-20% ferrite hot tears,
-crocks. and laps were formed. Annealing of hot-rolled and reduced tubes
av4-70-780C imparts a structure of granular pearlite and the mechani-
cal properties needed for further cold reduction. Metal consumption
for almost all steels, including machining. proved no higher than
those for similar pipes of stainless steels in current production
,practice. "Engineers N. S. Kirvalidze, R. A. Prudkova. N. N. Pil'nikova.
L. S. Rakhnovetskiy, 1. S. Pechennikova, and otherstook part in the
work." Orig. art. has: 8 figures and 2 tables.
ASSOCIATION; UkrainskLy n.-L. trubny*y institut
Research Institute); Pervoural'skly novotrubny*y
New Tube Plant); Nikopol'skiy yuzhnotrubny*y
South*= Tub* Flatnt)
SUBMITTEDa 00 ATD PRESS: 3045
SUB CODEt MM.IE NO REF SOV: 010
(Ukrainian Tube
savod (Pervourallsk
savod Oikopol'
ENCLt 00
OTHERi 000
Cord 2 / 2

L 98-74-66--
14> --p (z)/1.
ACC NRj AT5022779 E..A(c) JD/Ml SOURCE CODBI MV3164/W000/014/01D05/0010
AUTHOR:, Ntmnko, V Ya (CanAidate of technical sciences); Yermolovp T. V.
(Engr.)
ORO, VWXITP -
TITLE: Causes of formation..of scales on the outer surface of btainlus.-Iteal--
bot~-ronea Apoz
vs 8
SOURCEs Dnerropetro k 461 uwqy naucbno-1s9ledovat9l'8-k-1Y- --k0Dj5-tr*t0rsko-
LO
oy.,Ina 6!jnbqt!-- 12V045tvo
4
1100 SWx;niV istey yo tooril I RiMiCeArubnogD proizvodatys
(Collection of articles on the theory and practice of pipe production)t
5-10
TOPIC TAGS: p1paq stainless steelp hot rollft& corrosion
ABSMCTs Difficulties which developal an a 350 pive roiling mill'iroaucing stain-
p
less pipes having a diameter up to'325 = are demorlbed. Tbe inner surface of
those p109B met the necessary technical requirementag but the outer surface had
Cara

L 9874-66
AGO NR: AT50ZM9
serious defects In the form of scales, maie up of tbinp 0.5 to 1 mm films. May
could be removed only by mechanical processing on special machines ana by changlng
tbo al2e of the outer-wall diameter. In order to establish the cause of scale
formation unler Industrial conditions# an experimental Investigation of the
Influence of basic teobnologIcal factors on the quality of pipes was carrigrl out.
The InvetAigatton consisted of increasing the content of harmful alimixtures -
arsenic# losip tin and copper; Inereising the content in the metal or free aM
combined oxygen, hydrogen, ani nitrogen; ani IncrensIng the content of sulfur In
tho fuel used In the continuous furnaces for preheating ingots. The tnmpq-rature
scheiule of furnaces, the cooling of working rollers of broaching machines, ani
the wear of rolling tools were also Investigated* 7he analyses of thres.lealing
typos of steel were rMe and no trace of arsenic, lead, or tin were found. The
coFper content was about 0.Rj within the limit of requirements and did not influ-
ence the rormation or scales. The presence of geaes (oxygenp hydrogen, nitrogen)
in steel sharply decreased the plasticity of the metal and caused destruction In
the outer layers cluring the Swocess of deformation* It was characteristic for the
pipes with scales an tbo outer surfaces to have an Increased oxygen content when
compared with the initial Ingots. Hydrogen and nitrogen were within the limits of
Card 2/3

L 9874-66
ACC NR: AT502ZM
tochnical re,,ulromonts. The furnaces operating on natural gas fuel with no
sulfite admixture thus hal no Influnnee on the scale formation. 7ho r=qcas wnre
fired previously with fuel oil. When gas was substitutel for oil the furnaces
wore not reconditioned for the use of gas and the temperaturn schaiule
deteriorated* The metal ramained for long periols In hi gb-trmpara turn zonns with
a considerable excess of air, which caused overheating and Lurning of the outer
surfico and the scaling of pipes. 7ho cooling of broaching-machire rollers with
cold water (lid not seem to Influqnce the formation of soalne nor AH the wo.'Ar of
rolling tools. The following meioures were recommeti4eds Docrasse the totnl time
of preheating the Ingots to 10 - 12 min per cm of the Ingot diameter. Dearnise
the temperatures In the rirst zone to 1000 C1, In the second &one to 1180-1190 C;
In the third 2one to 219D-1200 C, Decrease the temperature of the Ingot center
when preheating. Explore the possibilities of conducting the preheating process
In a neutral or lightly o~ddlxlcg atno9pbare. Orig. art. bags 3 figures*
SUB CODRs // SM DAM none/ WR RV SM OD2/ OTHIMs ODD
cora 313

CBTXMOVAl I.B. (Loningrad)l BY77NSY.1y, I.A. (Leningmd)
Docarbooqlame a glutaxic acid. Ukr. biokhin. ektur. 34 ro.31456-
474 162. (MIRA 1815)

ACCESSION NR: AT3013136 3/3018/63/000/000/0-163/0'-73
AUTHOR: Sy*tinskiy, 1. A.; Avenirova, Ye. L.; Dementlyeva, S. P.;
Ostrotsova, I. B.; Priyatkina, T. N.
TITLE: Gamma aminobut)-ric acid in animal brains during radical
accoloration and narcotic -sloop
SOURCE: Trotlya Voesoyuznaya konforontsi a po biolihimil, nervnoy
sistemy*. Sbornik dokladov. Yerovan, 1913, 163-173
TOPIC TAGS: garamn aminobutyric acid lovel, aminobutyric acid,
glutamic acid decarboxylase activity, radial acceleration, cortex
Inhibitionp amytal sodium, chromatography, electrophoresis,
eloctrooncophalogramp central nervous system# beta oxidation
ABSTRACT: In the first of two series of exDeriments the level of
gamma aminobutyric acid and the activity of its enzyme, glutamic acid
decarboxylase, were determined in rats in relation to functional
activity of the central nervous system under conditions of strain.
In the second series they were determined In relation to the
functional state of the cortex inhibited by amytal sodium. For the
first series animals were subjected to radial acceleration of 23, 33P
Card 1/3

ACCESSION NR: AT3013136
and over 39 g on a centrifuge and then frozen In liquid oxygen.
After the brains were removed, they were divided into large hemi-
spheres and cerebellum for extract preparation by Robert1s motho(l.
Amino acids were separated by chromatography and electrophorosis.
Glutamic acid decarboxylase activity in the large hemispheres was
measured by Barburg's manometric method. Por the second series
animals were injected subcutaneously with amytal sodium to induce
narcotic sloop and then were frozen in liquid oxygen. Eloctro-
encephalograms were made before and after injections. Findings show
that gamma aminobutyric acid and its enzyme take part in the ros-'st-.
ance processes of the organism under heavy strain, Increase in
ga.mma aminobutyric acid level with radial acceleration of 33 g appears
to be a protective reaction which contrib~ttes to inhibition of the
central nervous system. In animals with induced inhibition of the
cerebral cortex, gamma aminobutyric acid level Is reduced when
brain blopotentials are sharply depressed. To compensate for this
roductionp beta oxidation of the gamma w~i!nobutyric acid takes place
and beta-oxygamma-aminobutyric acid forms. This is reduced when the
animal awalcons, Orig. art. has: 3 figurest 3 tables,
2/3

ACCESSION TIR: AT3013136 0
ASSOCIATION: Laboratoriya Ichimli belka fiziologichoskogo
Instituta im, A, A, UlMtomskogo Leningradskogo universiteta
(Protein Chemistry Laboratory of the Physiological Institute,
Leningrad University)
SUBMITTED: 00 DATE ACQ: 280et63 ENCL: 00
SUB CODE: AM NO REF SOV: 012 OTIIER: 0,29
Card 3/3

CSV*',TSGVli, I.B.; ~'1711Z;KIY, I.A.
I t-
,;dy of tr~c- 9'U'.R.Mic decarbey-ylare h!,t.vity in thc, L-hJr f~f
rats follawing the introauctlftl",f strychnine and '.--r.4cotlr-4c
arld hydrazide. Ukr. blokhim. zhur. 36 ... 4,5c,3-5W 164.
WIJ,A 18.12)
1. Laboratoriya khimli bt~lka I.eningradskogo gosudar',3tvCnnof.,'U
universiteta. Submitted August 25, 1963.

L MSAz-,C-2/M-Z/EE0-2 AFF7C/ASDASD-3/kKC PD-4
ACCESSION NR.* AP3004894 S1012016310001004/00S3100B5
AUTHOR: Borisov, V. A.; Oatrayko. G. N.; Panasyuk, V. S.; Yudin, L. 1.
7
TITLE: High-power -pulsed -modulator 0 for high-frequency amplifiers and
oscillators without long-line shapers
SOURCE: Pr1bory*1 tekhnika eksperimenta. no. 4, 1963, 83-85
TOPIC TAGS: modulator, pulsed modulator, h-f amplifier. h-f oscillator.
pulse shaper, long transmission line
ABSTRACT: Two types of pulsed modulators intended for h-f equipment in the
supply channel of particle accelerators are described. The modulators do not
contain pulse-shaping long lines and, hence, appear to eliminate many drawbacks';
associated with such lines. instead. a partial discharge of a capacitor to used.
Switching is performed by thyratrons. One circuit is designed for a power ampli-
fier I Mw with a pulse duration of 200 microsec and a repetition rate of 5 cps;
Card 1/2

Mom
L 17331-63
'ACCMION NR: AP3004894
,another circuit, ZMwj ;ZD0 n-dcrosec, and 10 cps. "T4 authors are thamIdul to
Mo Pe1r;DVs Who made a number of valuable suggestions for improving both
modulator circuits, and also to 1. A. Samokhinfor his part In calculating and
aligning the second circuit. Orig. art. has igures.
ASSOCIATION: none
SUBMITTED: 0 lSep6Z DATE ACQ: 28Aus63 ENCL: 00 -
BUD CODE: NS NO REF SOV: 000 CITHER: 000
Card -2/2

L U5642-( 7 FW1 I IN
ACC NRo AF6o2l62o- CA/)- SOURCE CODE: UJV0089166102610031()20610'-r-!o
AUMOR: Brudker, u. I.; Kiseley. A. V.; Kon'kav, R. G.; lia~~A~.A.; 4Uan&m&_V- I-j
Ostreykot G 141 Panas .; Petrov I L. I.; Yasnav, G. 1.
9T~kV. ~S V. Yud
ORG: none
TITLE: Starting of the D-3M synchrotron, used as an injector for a positron-electron
storage ring
SWRCE: Atomnaya energiya, v. 20, no. 3, 1966, 20-210
TOPIC TAGS: synchrotron,
A;= accelerator, storage ring, cyclotron mMnet/ VEPP-~ I
storage ring, B-3M synchrotron, ILIJ linear accelerator
ABSTRACT: The article describes an adjustment of a synchrotron with external single-
turn injector and single-turn emission of electrons and with a specially constructed
electromagnet. This pulsed synchrotron is designed to serve as an injector for the
VEPP-2 storage ring for colliding positron and electron beams, designed and described
by one of the authors (G. I. Budker, et al., in Trudy Mezhdunarodnoy konferentsii po
uskoritelyam, Dubna, 1963 [Transactions of International Conference on Accelerators,
Dubna, 19631, Atomizdat, 1964, p. io65, and elsewhere). The article describes the
synchrotron itself (Fig. 1), the =gnet, two variants of capture Into rjnchroniamp
and various test procedures. The Injector for the D-3H synchrotron was an IL1J pulsed
linear accelerator. The injected electrons had energy 1 - 1.5 Nov ("e duration
-7 nsec) and were acceleratod to 5D Nov. The D-3M synchrotron makes It possible to
2/2 uDo , 621.3%.6l2. 12

ACC NRt A16021620
Fig. 1. Block diagram of the apparatus of the B-3M eyn-
chrotron. 1 - Starting-pulse block, 2 electroragnet
excitation, 3 - hf generator modulator, 4 - Injector hf
generator, 5 - phase shifter, 6,7 - modulators, 8 wo-
computer, 10 - phase fixing block, Ll do-
plifier, 9 -
lay line, 12 - electron gun pulse generator, 13 - elec-
tron shutter pulse generator# 14 - inflector pulse gen-
erator, 15,16 - delay line, 1T - voltage comparison,
IS - reference voltage, 19 deflector pulse generator,
20 - electronic shutter, 21 channel electron supply
block.
operate the VEPP-2 storage r1r4g at energies 100 - IN Mev wA an electron current -100
mA, at an approximate repetition frequency I cps. 7be ILU Injector was recently re~
placed by one with hIgher Injection energy (2.5 - 3 MOV) and lor4ger inj*CtIon Pulse
(15 nsec). TUs increased the number of el*ctrons In the storage r1rG by &yproxia&te-
ly & factor of 10. 07340 67to 1"1 10 figures.
60 CODE: 2D/ sm wn , 2zwv65/ mm Fzr, oo6
LCard 2/2 '~/' -

ACC N;Zt A?7001936
AL-11-IOR
SOURCL CODE-. 106fiO746/000/006/0G39/0040
Grits, Yu. A.; Panasyuk, V. S.; Os-treyko, G. N.; Yudin, L. 1.
ORG: Institute of Nuclear Physics, SO AN SSSR, Novosibirsk (Institut yadernoy
fiziki, SO M SSSR)
TITLE: High-frequency power stage excitation circuit for feeding cyclic and linear
accelerator resonators
SOURCE: Pribory i tekhnika eksperimenta, no. 6, 1966, 39-40
TOPIC TAGS: cyclic accelerator, linear accelerator, particle accelerator component
ABSTRACT:
In high-power common-grid pulse amplifiers for cyclic or linear accelera-
tors, low efficiency and pulse distortion result from a mismatch bCLWCen
the driver and the power tubes where the second harmonic is undesirable
An excitation circuit is presented in which the fundamental and the
second harmonics follow different paths at the power tube cathode Input
circuit. The interotage circuit between the diiver and the power tube
consists of a tuned split LC circuit (tuned to the iundamental frequency).
two parallel cable sections assuring a high travelling wave ratio for
the fundamental and a high impedance for the second harmonic (cable
length is such that it acts as a quartcr-w4ve.c6ble .-or the second har-
monic). The second harmonic is further t~aoped by LC circuits between
uDC: 621.3.084-872:621.384.61;621.384.62

ACC NR, AP7001936'
the power tube cathode and ground. The described circuit was tested
using a GK-5A power tube operating at 6.3 Mc in pulsed mode. 71he out-
put pulse had a power of 3 Mw. Its duration and repetition frequency
were I msec and 12 cps, respectively. It is claimed that-the efficiency
of this circuit is 60% greater than that of the simple common grid cir-.
cuit.
Orig. art. has: 4 figures and 2 formulas.
SUB CODE: 20/ SUBM DATE: 02Dec65/ ORIG REF: 002 / ATD PRESS: 5111
2/2

jtt)- j~LxlAt,r G. I Votived'ov P. I - ; Voptovoy Yu.A. Nolbovonko.O.A - ):a I kdov A - D -
"It rey%~~. ; Panany.kV S
i I Thip W-D turn oynchroti-tIn
Ait.trtutl tokhnicheskoy f1rAkI , v.:11i I fill. 1), 111rih,
7AGS: oltictroa ficcolorntor, oynchrotron
A 74 1 1;-, r I a C oncO r ned - I t h t -, X y I., 1QJ4 I r on- f r a 1 r n
.,d It L t ~o I Y aj' CU A.N rj.'; rR f r L nj t i -, o ( .1, to I it 0 !,!,,V v 1, t r n.
t ;",: .A W ; 3 1 1 J ~ I " ~ r It L Il It ~ f t 4 111 1 11 t - 1, z, I I , - " f I I ~ I V I, r, I. I..
,'.orn~.;y in fial otbnr -Cli(irs (Trnn,.n,t L,,m, Of the Int-t-nit 1-- , I
Acc., 1-~ rntorn 3uh-in . Vt63 , p. 106f, , AtonIzAla t , M . , ;'1,,4) . I n LA-
.''It., "I of t;.o accolerntor are deacr L(A:d in -.Ot~-whnt r4orv tint it I , I T-.(- Lr,;~. t:.,,
,-L, tho ma,-.n,,t p-r &.pply, aml tto Injoctor, alld th-3 of [t- 1, , ~,,
,I I In . 7ho raa,-,not w1rulin,-, con:ilsto of two concentric rL:,, . , ~
Uio lx~t= circulatori. 7he outur ring, In capable of
50 at=, arki thu geozictry to ouch that the Inner ring Is In
not ic I orcoe , IxIlni: a ubjocted only to a hydro3tat to pressure. 7-~ Lza,:-
by a 0.045 F capacitor bank charged to 10 W. The maximum coGnot currs;;t 1- ii-out
Co'd 1/2

c--- --l ist:- to -i ~Iocf rtlo -Int 1-v ~f III() VoV . Tht, n t~ t I t
it 0 1 , 'I' 1 1, 1 ;-*. It Or t 1-
C- 1.,J...:t 1,I.1 (If GOO IN o]--I I-,
Ik ,vo I I, k I It ( Iw v opt m-il I, l-it rolit-i Tho 1; 1- )1,, 1 1-
I ol. I o I lo-I I It (11. 1 Im f lo 1.1 1 0 I'l . I - I ,, , I . - I )-
'..' r f nc, r n I 10,1'. v o I t n flo LI fre(Itimwy Irmi I it I
'-,I t I) Ov I-o,m It i Lit tlko nid Of ,I it liij-,Ict r*v!iV-tnkOr lit tit I, it -' ?n''.
t 1"0 lie 0 t ... I .' m,, I I It t J- ,, I j o -, I j. I, t of t 1, 0 -, C I I k I I(, I Ito t .n,.,~ f . -
L wn I ;)n!, n I I) to t f) J iij ot: L abou t 1 .2 A 4); 600 1 V V I , 1: L r Opt.: t) 1,q
cot, -1 mt f ltlO tn nrc,~ to nann 2o :~ or Lit,, I nj, , t,
Cm-y")'It ",t I fomwl to Ito I by lo-~ Lt..] I ml p-c- , I",
0 C 17--0 1 rAIL11111' t1inji by I. rowivorno cloo;g, Own, rc, (~,' r-
L-I 0 10-:1oir ctsrl-ilttl 0 (171%t b- nChloV,A With n ntrarl I ....
I -,. vto witl)or-) th,,itit h-A-N'-,1-Iyv for )%I,) li%tem'it myj
OrGn,jJLzIvj: Lho fnfirl.cntion of MO Matil IIIII-I.Pi (Ii 0- mcv'-,-vAov
pnrtlcipntl.v,- Ii. L~. I
~,t vi col-Lain parto Ojr tho nccolorator. Orig. art. has t 3 formulniti oul G I
]iUD C03M 20/ SUBM DATUt 273op65/ ORIG IMIN OOID/ cTil In-11: 001
Cord 2/2

ACC Ni( % -~ -,,,) (~ -i o L) 5~)OURCE CODE:
AUTHOR. Grits, Yu. A., 06treyko. G. N., Pana5yuk, V. S., Yud;r., 1- 1
Ol~G: Institute of Nuclear Physics, SO AN SSSR (Institut yadernoy liziki jU AN
SSSR), Physico- Technical Institute, GKAE SSSR (Fiziko-teklLniche8kiy inbtitut
GKAE SSSR)
TITLE. Hi,~h-frequency pulse generator with 8-Mw pul8co intended for a
power e1cctron accelerator
SOURCE: MezhvuLovskaya konferentsiya po ciektronnyrn u sko rite iyarii. 5t:i,
Tomsk, 196-1. Zicktronnyye uskoriteli (Ellectrun accelerators), trudy koniercrittll.
Moscow, Atomiz6at, 1966, 287-290
TOPIC TAGS. pulse generator, electron accelerator
ABSTRACT; A linear accelerator with a 40-amp, i. 3-Mev, 1
7-r,sec pul6c was developed and built in the PhyL;1co-Technical lnbtit~ite, G?"~AL'
SSSR. It was put into operation in the Institute of Nuclear Phyaics. SO AN SSSR,
an(i has been used there for a single-circle injection into an electron riynchrotron.
Card 1/2

AGG NIR: AT7004005
F energy btored ir, a o. I - Mc resunawr is
wised tor particle acceleratIOTI.
Mc)(Iulator I (see figure) t3upp,ieti vo,lage
pu:scs to two-stage generator 2 anoues,
feedback is effected via high-Q loau 3.
adjustable coaxial line 5 is employed for selecting the feedback phase. A low-
power Oscillator 4 is intended for overcominr the resonator multipactor. A power
of 8 !Aw wan obtained from the generator, with .5-kv anode pultieti. (laring Iriitti.
However, in the above high-Q-1oad -excitation scheine, the generator develops
3. 6 Mv at 16 kv. "The authors wish to thank A. A. Naurnov for orpanizing th-is
project. and V. 1. Vishnevskiy, N. P. Rubinshteyn, and Ye. P. Mcl'nikov for
their participation in the alignment of the equipment. " Orig. art. hati: Z figures.
SUB GODE: 09 / SUBM DATE. 06Mar66 / ORIG REF: 003
Card 2 / Z

SAVIC, Isidor, prof.dr. (Beograd, R-:3ar-ska 10a); OSTRIC-41ATI.'ASEVICS
Biserka dr inz., strucri sarad.-.ilk; IIA~SIXOVICC, DoC--wr,
riMfl~js`aradn Lk
Lyophilization of ment. Telmika Jup IP no.7tSupplementl
Prehrar. ind 17 ro.7tl340-1344 J1163
1. Rukovodilac Laucne I strucre pro~dem%tike Ir.stltuta za
tehr.ologiju mesa SFRJ, Beograd (for Savic). 2. Ingtitut, zn
te$-vnologlju mesa SFRJ, Beograd (for Oitric-Matijasovic,
Maksimovic.

OSTR111ANSKY , Lubor; PANENKA , Jaroslav
Effect of nuclear fallout an the radiometric field r-easure.-
ment in prospecting for radioactive raw materials. Jaderna
energie 10 no. 2:3)-39 F '(-A.
1. Katedra tizite geofyziky pr1rodovedecke fakulty, Karlova
universita (for 09trihansky).
2. Geologricky pruzkum, Jachymovske doly, Spisska Nova Ves.

O',;TRIKC)Vp M.S.; VITKEVICH, N.D.; SVIRSKAYA, O.D.
Kinetics of the iricrc~ase of shrinkage stresses in systems
undergoing drfing. Koll. zhur. 23 no.1:122-124 Ja-F '61.
(MTTI A 1".. 2 )
1. Rostovskiy gosudar.9tvennyy univeraitet.

SVIRSKAYA, O.D.; OSTRIYOV, M.S.
Shririkage stresseg In a --- - - . I . "" I ters. Koll.zhur.
26 ,.1,95-r49 J.-F " . (MIRA 17:4)
1. Rogtovskiy vinlv~ral.* , tot.

DIBROVS. G.D.1 OSTRIKOV, M.S.; PETRENKO, T.P.
Contraction (setting) of cenent stone. Dokl.AN SSSR U9 no.3t
648-651 Mr 163. (MMA 16t4)
1. RoetQvakly-na-Donu inzhonerho-stroitellnyy institut i
RobtovsAy-n&Zonu gosudaretvenr47 universitet. Predstavleno
skadexdkom P.A.Rebinderom.
(Cement)

PALKIN, A.P.; OSMIRIVA, N.V.; VIMITOVA, TON.
Interartion 'n the 1TYutem '~nC13 - In . Zhur. neorg. kh'.m.
n0,21:2566-'568 N 163. (MTRA I": I ,
2. Voronazhrkly go.~mdarqtvenr-yj universitet, kafedra
noorganicheskoy Oitmii.

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AvIvatmal Cultivaticn,'" :,. I. mmyarevald'y
s3idrotel& i HaUcP Uo 6, pd- 7~-~
:jui,in,] 12 - 11. ~ar in ;:~- scjw, u*.,I("
Union Acad of .,,-ri "ci im,-mi 1.(,n;n hel,ll a Icnizi,
and hydroloL-;ical aLln-Istm-tors, liroctom, and :-klill
tractor stationo,', besidez; precdents .' Ioll~iozo in irri,-ated
and Saratov in Oblastr. Di7;curscd ,.,cre roblems of ut-,'--*z.4n,;
c ~~ndi'.ions -.et 'lie ',',) 1,-a a::(i In -)'.hr~ r nrvi re -i on:-, to i m-, i; ri, -a i.
hearl fron 2.1 lecturers.
i'A 227746

Oskmu, Eva; WAZINA, Krystyna; MARKIEWICZ-CZAPSKA, Danuta
A ease of encephalitis following vaccination against rabies. Neurol.
nourochir. pBvchiat. pol. 12 no.1:123-126 162.
1. Z Pracownl Warazawnklej Zakladu Neuropatologil PAN Kierownik Fra-
cowni: doc. dr E. Osetowska z Kliniki Pediatrycznej AM w Luhlinle
Kierownikt (prof. dr W. Klepackil z Kliniki Neurologicznej AM w Lublinie
Kierownik Kliniki prof. dr W. Stein
(RABIES immunol) (VACCINATION compl)
(ENCEPHALITIS etiol)

OSTFOV. X D
Spravochnik po radloizmeritell rWm priboram. (By) K. D. Osipov
(1) V.V. Pasykov. Moskva, 'Sovetskoye Radiol, 19 -
V. illus., diagra.. graphs, tables.
Contents: ; v. 3: privory dlya lzmerenlya
forrV kolebanty; v. 4: Spetsial'rWye izmeritellnyye pribory i
istochniki pitantya;

zX%GA1JW.'1?T =ICA I-C.6
2214. IJAEMOPTYSIS IN PERIARTERITIS NODOSA (Russ ian text) 0 Is tr a kh
D. G. and Mochalova A.D. - KLIN.MED. (Mosk.) l95T._35_T4_C1_ i-3 -
1T9T_1_Uus. 2
In cases of periarteritis nodosa the lungs are seldom injured (in 12-251,v' of cases).
In such cases the vascular process in associated with the development of small
fibrinoid pneumoniae. fresh haemorrhagic infiltrates which show haemorrhagic
tendencies. A description is given of one case with a fatal issue.
Frey Baden-Baden (XV. 6)

mmomwo co ftAwom bum dib~
omdmh* MOUSUM ke Owks MUMMA$ op~"
ad w a. modabKophWA - S 1, IN nncr. M If fhuiuukl,
&YO 11 S Twit (j a/,/,I Phys. 1932.2t ISK-20' 11ir .%I, ul
SIM" hAvr fwrn nUkir IM 13,1111-OWHAPF"ng nnatitinal linv% asing
a 41,trmsim Ifirmilla fm tlw line-ohmpr "pn-ntAtl.,n Vw. 4 tilt-
bral &%mism? rxlwflnwnf3l data on lntRjrmt14I afft,11,11on And
it4m, kmal Inlo,-will, ha,ilt it, r*1tuIAIt,I rmsuoviim~ villub at- in
sriminwnt With r1tral"Wr'd emprical data PuNW-1 by
IfiAtri arml by Vitnth In rdt"W'dAY. th~ th-n-titAl (1#jWniIrn,V 1-1
,FIUYMV%ty oft fililLad dinwity. fur iiniall optital d4mam, at :tilt$' K
Ilt"Ll,N)p The takillsium of vinhaiviors can 1w SIMIAIN'l by tile
.- 14 All*"% III-21"WI)IN r If Xfoolm
7,Y.