FR:REALITES MALGACHES TO:UUCONNEAU F.

• Document Type: CREST
• Collection: Consolidated Translations
• Document Number (FOIA) /ESDN (CREST): CIA-RDP91-00929R000200820055-0
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 98
• Document Creation Date: December 29, 2016
• Sequence Number: 55
• Publication Date: December 31, 1983
• Content Type: ABSTRACTS

The Cancerogonic Action of Radiations and
VirtINOS Oil C011S GILItiVatCd in VitrOp by
Diego Balducci.
ITALIAN, per, Recenti Progressi in Medicina,
Vol 38, No 1, Jan 65, pp 42-59.
MIRS CSO: DC 12942
S-351/67
Sci-B&M
Mar 67
321,880

Dioxyline Phosphate for the Treatment
of Certain Vascular Syndromes, by
U. Milia.
ITALIAN, per, Recentia iAedicE,, Vol 7,
No 12, 1968, PP 5469-5498.
14T0 72-11010-060
May 72

1~%Ii sym3?o9icw of 1.,loctric Group of &,or,
by Guy Ringenbach,
rMNOis'Por, 11.0coption du Laboratoire
d4hapesantaur. July 7-13, 1966
"qASA. -ITF
Sci - I-I'Icc
i
'we,. 67
C,

il (- (!,, (utiprranw-293) UVrRACENTHIPUGATION: A
COMMERCIAL BUSINESS AND A POLITICAL OPERATION,
Malleroy, Antoine . Translated by H. W. GrDenswegen JAUB-
tralian Atomic Energy Commission Research Establishment,
Lucas Ifolghts), from Rocherche (Parts); 1: No. 1, 77-80(1970).
7p. Dep. NTIS (U. S.'-b~a ~esy).
isotopes; translations 18D
MN-22 NP NSA
0

Saclay Researcher Discusses Nuclear Analysis,
by Charles Engelmann, 16 pp,
GOVERNMENT USE ONLY
FRENCH, per, La Recherche, Faris, No 19,
Jan 72, pp 2 -34.-
JPRS/L 4079
Mar 72

J
L r
L t'

Structum MMY'VtOUVO do* rjumM 11 lbr 66
coufte lindt's Imajoasre, 10&Uwm d I une
kri CIOAD Framu , hypersoravn
Frm: %A MOMM AMOMWUU *W-jme 3.965 P93-10
( 8 py)'
rranch - ant fAr vdo:
Type I origiuma and 1 carbGn mpy.
Mcmnt bay be mt.

Re-AttachemeiTt of an AA-Syimetric Supersonic Jet on the
Wall of a Co-A)dal Cylinder, by J. Delery.
FRENCH, per, Recherche Aerospatiale, no. W~, 1965, PP 15-
20.
NTC 7o-16996-olA

Ignition of Hybrid Rockotspby M. Barvero,
PRENW, per, La Reehopdw AerosEat.11100
No Mg pp 33-436 IM,
Dept of Navy Ty 4726/APL/JliU T-1791
Sci-Asro
Jun 66 302g,094

Streamlines in a Continuous Flow., by
Robert Legendre.
FRUNCII, I)or,, La Recherche Aeroseatiale,
No 105,, 1965S, , =. 9230046
MASA TT P-405
WE-France
Sci/Engineering
Jan 66
2930185

Minimum Fuel Ortrital Transfers, by
Jean-Pierre Maroc.
FRHNCH, per, La Recherche Aerospatiale,
No 105, Mar-AFr _19657.
CIA X-6932
NASA Sci & Tech Info Facility
NAS-8-21091
CFST1
Mar 69 577,258

*AIR=-FoAI Orbital Transfersp by
J"n-Plorro Maroop
aovzumw = ONLY
liale
MOK26 perp IA Recherche Agrog
mWiale
No 105, 1965,17-11-a. P2D010Wb7
Rsic-500
Sol-Aero
ft 67 326,0166

Study of Critical and Limit Rougbnesop
by Z. Vaucharet., J. M. Olive. 17P.
FOR OFFICIAL USE 01W FOR INMMAL USE
WJLTEaN THE DEBkK%= OF D&TEM MU
FRECH., pert La Recherche Aero!4~ialep
No lo7, 1965, pp 33-36. p loolo3b66
FTD-TT-66-32
Sci-Aero
Jon 67 316:363

A 1-~)thod for the Nandispersive Amal~sis of
Vory Light Hlomisits,, by R, Castaing,
F. llicltoir.
1:10401, per,, Modi Aprosput, No CVIII,
1965, pp 3-16.
NIGA TT F-422 -
Sci-E. Sci
Au,g 66 3080909

Experimental Study of the Combustion of
Ammmium Perchlorate Spberes in a
Gaseous rvel Flow, by " Nadaud,
FRENG1. per, La Redierche A*M!patiale.
No 108# 19050 pp " I*
Dept of Navy Tr 4747/APL/JHU T-1816
Sci-Aero
Jun 66 302v195

The Principles fif Global Vibration Tests of
a Structure, by Go do Vries
FRMai, par* Rech Acromato NO 108,
1965, pp 57;61-.
NASA TT F- 10,003
L c. -7,-26
U. So GOVERNMENT USE ONLY
Sci-Engr 2980644
Apr 66

Proo"U" fOr tb* OIGW Ylb=Um
2*4 Of lk BtZUattins by C, Bfttftz*
YMC4 P;g!MML*~~jaU~ No .109.. 305.
ML Rof :
Sel/Pt"
Ap r 6.9 380~235

Wton-ainatiml of t1je Glass Tronsitim Tomperatum',
of u Plastic Matorial From Tho Variations in It$
I
"undul,
ur linritiuss, by 3. Porsoz, Go Cranior,
F11-NO1, por, Rech Aerospatiale, Vol XCIX,
1965, pp 11-16. 17-~O
MA,
I SA TT F-365
sci-.11/11
Jart 66 294,535

Spherical Rocket Motor With a TWo-Componant
Solid Propellant, by P, Larm,
FRENCH# per,, Rech Aeroppatiall, No 109,
1965, pp 21-ZT.'
Dept of Navy 479S/APL/JHU TwIS2,3
S ci - Ae ro
Aug 66
3050646

Unear Pyrolysis rato of Anmium Perchlorate
in a One-Dimmsional Flow* by M, Gdnet
FRENOi, per, La Rechardto AarqUatials,
No 1096 19650 P; 41 9.
Dept of Navy Tr 474S/APL/JHU T-1791
Sci-Ae"
Jun 66 302,193

Solving ampUfled Equations of a Tmtul4ut
Viscous &=dary Uyer idth an Amlog Coqxter,
by Jmn D&1=7, 12 pp.
FREUCH9 par* 11poh La 9 1966* pp Ic.,.18*
P9U(IL7068 M, No UO
AW--SC-T-67-0935
Sci-~Ath
Mar 68
349.332

The Investigation of a Principle Applicable to
a High Sonsitivity Accelerometer, by Michol Gay,
12 pp.
FREN01# per, La Recherche Aeros2ttial, Jan/Feb.
1966 No. 110, pp 39-44
P944347167
TIL 1174
Al -r e, - 617- 13-~ 0 3-0 / L)
WE
342t428

Naw
LA MCBMW
w 19v M-30
41dad b7l OJ.R.B.&
ANaft . aft for V"3
R4bT3U-o
lb. 2u lb 5 Aus. 66
*NO-&vrU 106
( u pp
TX*Ma&U Vad tMj arIgL=a COEW.

Derivation of Natural Frequoncios and Modes From
a Resonance rest Using lnq)erfect Excitation, by
D. Clerc.
FRENCH, per, Recherche Aerospat, No 111, 1966,
pp 41-52.
RAE 12 B
Sci/Electronics
Jun 67 329,202

Study of the Aeroela3tic Instability of a
Flat Rectangular Panel, by R. Dat, et al.
REM,, per, Rech. Apros No 1129 19660
. Pat's
pp 27-32.
NASA TT F-10,645
sci-phys
Jul 67 331o�94

Influence of Prestressing an the Streught
of One-Dimational Laminatess by M. Hadiud,
PIMNOI, per, Rach. Aprospat No 113, V660
. P
pp 3.6,
NASA TT P-10,909
Sci-Phys
Jul 67 331,70S

Onern Trajectography Trajectox7 Restitution
without Any Known Wtial Point,, by Robert
Galarne, 22 pp,
GOVERM621T USE ONLY
, per, La Recherche Aerogpatiale No
113# Jul-Aug 17 =)PP- 15-23,
JPRS GUO 2114
WE-Fi-ance
Sci-Ordance
Dec 66
314s.127

Study of a Family of Diffusers for Low
Roynolds Number Hypersonic Wind Tunnels,
by B. Monnarle.
ITALIAN, per, Rech Aarosp!t, No 114,
1966# pp 9-16,
NASA TT F-10,876
Sci - f4ethods & Equipment
Jun 67
326,085

The Ablation uf Solid I-tiols used itt itybri.L! I~ocj,~ots,
by Lionel Notlaud IS Iuwi lilasilij, 15 iy.
(;Uvyo lkiii uIldly
FRIE-NGIA jv--r, La Radiarcho ixoros~zitialc, No. 115,
1906, pp. 45-55.
MIC 717
f, Facls 342,429
Nov 67

Visualization of Combustion in Hybrid Rockctsp
by Limiel Nadaud, JOMI Hinsini.
FIZEN01, per, w itacherche Aer2!L!tialo NhIl7j,
1967, pp 3-19.
WAC-716
(I .."?
"OVEIN"! , -* *41F USE (INLY
Sci- Prop (11 Fuels
'lov 67 344*670

ooo"'"A~ to um otuv at go ombwt&m of
AlValwa PUU&2~- W AM %Vbr4; 43 IV?
FMOM4 0 39? ,p Mkor ilso
jpn Goo
ML4*=N
8400m 1
4
339#47

COmPar4tiVe Study of PwZe for the First Stage of an
Atmospheric Booster, by C. Bust. 22 pp.
FRENCTI., per., La BechercholewaLaligle, No jig, 1.967, _
pp 3-12.
AIRIFTD-HT-23-891-70
DISTROUTION LIMITED TO U.S. GOV#T AGNUTES ONLY
COPYRrGHT INFORMATION
=q 71

p"Cise mossuvomt of voloaties Vain a I"or
latwferowt4r* bW isma-Plem MLon.,
FROCHO PWO JA R!2Mnb2 AMEMS"a so U99
1967a pp 51-56, -
Dept of Favy/APL/M T403
Sol-Pbysim
Doe 67
3469600

Artinvial Irdlistion of the Supwwfda Tissudtims
1:~r X. Vauchoret.
FMCHS per$ 1A Rooha9to Aarowmt&at, No 120g
196?# pp 25-32.
XAS& TT F-1111CM
.Z
Sci/Pbye
Apr 68 351o433

The Use of Semiconductor Strain-Gauges for
Measurerement in Hot-shot wind Tunneks,
by J. M. Darmon, A. Devacht.
rRLNCII, per, Recherche Aerospatiale, No
120, 1967, pp 43-49.
NLL Ref: 5809.95 (T.6084)
Sci-Aero,
May 69 380,683

Priming an Air Inlet in Unsteady Flow
At Mach 7, by Sean Pierre Bourgeois,
Otto Leuchter.
GOVE-iiiTlIcAre USE O"TLY
FIH!'11CH, per, La Ilecherche Aerospatinle,
121, 1967j, plo 13-15.
~-11T P-11,665
sei/rj~~ero 368,970
oct 68

Tests of Rocket Throats and Nozzles. by
Jacques Nicolas. 15 pp.
GOVERNMW USE ONLY
FRENCH, per, I& R9F_InXLh.M Aerggpotlele,
Paris. Jan-Feb 68, pp. 21-28.
MRS GUO 2771
Sci-Space Tech.
April 68 355,827

An Analytical Approach to tho Problem of
the Accessible Domain of a Ro-entry
Glider, by Jean Fave.
FRENCH, por, Recherche Aerospatiale,
May-June 1969, pp 3-11.
.NASA TT F-12,158
Sci-Aero
June 69 384,129

Heat Transfer in Liquid Nitrogen in a Zero-
Gravity Field, by Jean-Louis boulay, 36 pp,
FUNGI 0 Perg La IWchumho Aerospatiale No 122,
1968, I)p 35-50.
AIZNI/RSIC/Tr-855-68
GOVEMMENT USE MILY
Sci/pIly
Doe 68 354,946

-Application of Synthetic Plasmas to the
Simulation of Space by Jean
Kapriklian, Jean Labbe, &dle Le Grivau.
FRENCH, PER, la Recherche Aerospatiale, pp.
41-50, July-Aug 1968.
LL (135)-69-253
Aug 69 c, 5

"'Gatf-cm, of lkaosraWbU
Vlnd ftwas.. by Klebal adl in
bwtp Joan sumt.
jmms pwo Awoo
3010 DoUals.
o 2966p pp 172-00.
BRA of Nay XwVJW T-9R94
Sal-Pbvu
svt C9

Ott.-Board Solid Noon Cryostat Described# 1w
Jam law-onto 5 pp,
GOVRRNMT USE ONLY
MNCHI, per$ W Rooborche Asrospat-lalet
Pariso Nov-Doe 1968o pp 61-62,
JM GUO 2970
Soi-Space Toch
Mar 69 375083

Optical Rocket Orientation System Necribeds
tW Jam Surget# Claude Vorete 7 ppe
GUMNWT USE ONLX
MUCHg pw# IA RephardA Agrositialos
Paris& Nov-Doe 19Mp pp 62-646
JPRS GUO 2970
SGI-Magne Tech
Mar 69 375t9M

Solid Propellant Ignition - Geneml Comidera-
tionss by 14. Mu"re.
M-In I a AGE2MLMA10
110 323s, M ra ResbsEsbg
,v pp 15-2 B.
Dept of Navy APIPITU T-2179
Sal/prop & vvels
11
40V 68 368s529

fixperimontal Setup for Studying the Igni-
tion of a Large-size Solid Propellant
Grain, by Larue Pierra.
FRENCH, per, La Recherche Aerospatiale,
No 123, 1968, pp 29-43.
Dept of Navy/APL/JHU T-2286
Sci-Prop 4 Fuels
Aug 69 388,708

Measurement of ileat Fluxes during the
Ignition Phase of a Solid Propellant,
by Monique Scagnetti, Joan Crabol.
FRENCH, per, La Recherche Aerospatiale,
F-
No 123, 1968, p 45-i~l.
Dept of Navy APL/JjIU T-2257
Sci-Prop & Fuels
May 69 380,951

Analog Coq?mUr Sta4y of Vm IVItIon Pbses
of a Solid-Propellant p4o)wtp by joel Sin"I.0
.~ per, ZA Rosharww AMW-UAIA No 223P
1968., pp 63-79.
DIVt of Navy APVJMI T-2310
sci-prop & Rals
Oct 69 393,P331

Bmaocrpt&Lb)gmphLc st1w of .the Straeturo
of a Cuton Moodde Cqodepnits by R. Gnrt,.
I I Mao per, FAwb.&Hpmtlale No 123y 1968s
pp 81-84.
MM 2T F-22033
Sol-cbem
NOV 69 395.#T80

Photogrnphy of Lnser Botuas Rof looted
From STitellites, by Goorgos Jacovlev,
7 ?,P.
PREITCHI, por, La .11echerche Ppromatiale,
'70 123, 19681 PP 5547 *
Dopt of -.Invy APrIX,,IU T-2161
F
368, %2
Oct '08

1!:)qje4rmntal b-iwzti(jaticn of a Cascade in a
SitisdAc Nmular 4ind Tunnel, lyl J. Paulal,
G. Jansselis. 17 pp.
PIONCII, par, IA lbdiardw hoLojsmtiale, No 124,
1968, pp 21-2'90
,U10-7D,40-23-40-69
sai/aermautics
cbc 69 397t386

Interforometric Study of a Mach S Flow
Around a Sphere, by Joan Louis Solignac.
PRENCII, per, Rech Aeros2atials, No 12S,
Jul-Aug 1968, pp 31-39.
NASA TT F-12,121
Sci-Aero
June 69 383,208

AppIloation of Studies of Weak U=Lnmw
Fluns to the Optiml Beteation of laser
fth and tj~, the CharsaWrimition of opti=1
Cobere=j by Joan BoMot.
PFMM.o per, la Reaberobe &MMEN.Masip
No 125P 1968: pp 53-W.
Dept of Navy AP4-/JW T-2313
Sci-Pbya
Oct 69 393P334

Predicting Flutter in Dry-Friction
Aircraft, by J. Periaux.
FR:~NCH, per, 1jechel:che AerosTjFttiale,
Jo 125, 1968, pp 67-73.
14T0 72-10970-010
L L. U3 Lj ) .- ~q - ~'S. ~_
May 72
39-91 'S~j

Calculation of Subsonic or Transonic Airfoil, by
R. Legendre.
FRENCH, per, Le Recherche Aerosgatiale No 126$, 1%80
pp 3-13.
Dept of Navy APL/JIIU T,-2407
Sci/Aer
May 70 4079105

Flows with Simultaneous Natural and Forced
", I ~. , ~ f k !. ~ ~ /"J'4
Convection, by R. Kh. Zektounian. ,
FRENCH, per, Rech Aerosgitile,, No 227, Nov-))ec
19689 pp 3-9.
NASA TT F-12,254
Sco-Phys
Sept 69 391,S47

UnDtOady Supersonle AM AYMnd a ran CircuUr
Cylindar.. by Clabrj4d CoWy.
JRMM,, per,, Im m9mrabe Aeronatlale NO
Ins 196% Ipp 37~.43- - -
Dapt of Navy APZ,/JiM T-2299
Scd.FM9
Oct 69
393P93M

Talmstry Data ProcesaLng of the Sol* Project,
by Pq Raboult 13 ppo
FUNCH, per, Rech AerospatLals Vol 8, No 11,
1969v pp 1-50
NASA Tr F-42,883
ScL.?Elec
Jul 70

Aemsible D=In of a He,-entry Glider.
Gradient Method, by Joan ftva.
PFMM,, per., Rech Amm-atialey No 128,,
Jan-Feb 190., pp 3-16.
MU TT P-22,,4oo
sci4m
Oct 69 391.424

Xff"t of mmaidenoe and PAynolft Number on
olpentanic Flow ftst a Clraular Cons, by
AWas Valowd. 21 pp.
PFXWS6 per, Bach lalop lb 228.0
Jan-hb 19690 pp 1T-31.
UM TT P-3.2,401
Nov 69

Veloolty MxWbutlons in a TurbuUnt Bouniery
lam in adfam or Aceelomted Cowmselble
YLowl by R. Mlobelj C. Qu~. 28 pp.
GOVERNM USE ONLY
3212=, per, Bwb Aerospatiale, No 128j, Jan-Feb
imi pp 33-4T.
MM TT F-120538
sai-pbys
Jan TO 399,vOZ

by Anslog Simulator., of the
QYlinder Wake Potent4al in a 0011.1slonlaw
Plasm AXPU-sorda rJaw, by
COMM Fournier.
IEM=j, Peri Bscb &MMLS-Kae MD 328j,
Jan-Feb 1969,
pp (
MASA TT F-12j.402
scki-aws
Oct b9 393; 41.1

In-Flight Synchronization of Awdo Clookso
by Joan Beason, U ppo
QQURNMT USE ONM
A. i*A6.
FRLOCH, per, IA Roche he AaronLtial
Mar-Apr 1969, pp-48-52.
JIIRS/L 3093
Sai-Nucl Sol
Avg 69 3909423

AerodyamLe Coefficients for Control Surface-Tab
Coupling in SubsonLcs BidLeensionalt Unsteady
Flow# by R. Dot. 8 pp,
FRGNCHv part Rech Aer*sRt No 129, Her-Aprp
1969, Pp 60-63.
NASA 7T F-12,829
ScL-Aero
Oct 70

Dotanninatim by-N " Mthod of CMh tics of
.75Ai8r3CaC FlCW13-NA)OaaW Ilith a GLVan PraS UM
Lew p by Pier= lAzinger. ;6. Ippe
RE=j,,perj, Fudis-bqRLp~ale,, No 130,, 1969,,
I~p 3-15.
NASA 'IV r 12,,784
sd/physice
mV 70

Determination of the Vibrational Chstracteriatica
of PL Structure by Means of tha Exprenaion. for
the Applied Complex Power, by E. Bonneau,
F REN CH, per, Recherche kerospatiale, No 130, 1969,
pp 45-51.
NTC-71-12422-20K
Nov 71

p_geudo-Vi-accaity Ibthc)d and -StarLiny PrCx]E)SS
in a k1ozzle, 171 Pierre lavaL 28 [4).
171MG1, par, La Bodio ~Le~.)atieie, No 131,
Jul-Aug 1969, 71?- x--Iz
wv-A 'IT F 12,863
sciAilysics
r.W 70

A Calculation Method for Wings in Steady or Un-
steady Supersonic Flow, by J. M. Brun-Gabriel,
26 pp.
ERMCH, per, Rech Aerospatiale, No 132, Sep-Oct
1969, pp 3-13.
NASA TT F-13,033
Sci-Prop & Fuels
Sep 70

lordrogen Peroxide Use as Qddizor Describedg by
maurice fuglbstg Ifolone Moutot. 38 pp.
GOVEMMMT WE ONLY
FMCH9 per# la Recherche AerosR&~iale, Aria*
Sept-oct 1969, PP 15-31-
JKS/L ~223
V,e't -~w r,- f- /S
Sci-Space Tech
Jan 70 39?oB19

Now i'Acroprobe Analyser for Very Ught klommts,
by Pierre lanusse, 20 pp&
GOV MW U-T USE (MLY
FRENCH. per. La Recherche AsrosaVmlo. ?aris.
Sept-Cet 1969, PP 33-W-
JPRS/L 3225
sci-flucl sai
Jan 70 397,820

liamnic Abratim Tasting of a um-linear
Aircraft Stnctuw* by C. naftrix. 7 pp.
F7=010 per$ Fbdl. AgE2Watialee No 1320 Sep-Oat
1969, pp 58-59.
NASA 7T F-13035
sci/aeranautics
aug 70

Propulsive Evaluation of a Ramjet Installed
Under a Win& Up to Mach 79 by C. Rust. 26 pp.
M-2M, per, Regh AqV04RgLtLslgv No 133s
Nov-Dscg 1969p pp 3-14,
NAM TT P-12,951
N I C - 143 t- I - a C' -0
SCL-Phys
Oct, 70

Calculation by an Integral Method of the Laui-
mar Boundary Layers UWer the Xffect of an
BatzWy Gzaftestp by
G. Kretsechmar. 27 pp.
FROM . per . - A~ No 133v
NOV-Doe 19699 pp 13-27.
NASA-27-F-131plV
um
wA-a*xO
nov 70

r,apzusmt2ticn of a Ufting line in am A3dbitraty
modcn yy a lina of NnUaration DDAAats,, by
rcnald Dat. 19 pp.
FRDMO, per, ltdi. Ae!M2gtia-le, No 122t Nov-03v.
1969 # pp /%-t)
IWA Tr F 12952 -~ "~5
sci/aarmauties
aug 70

Applicatim of Elactrat Acrophcnes for measurrm
ment of Prtmsuxt3 FIvowtuistiam Cn lorodynautc
Profilesl, by Remard Sm" 7 pp,
FRMal, pers, lbch, AeMMatiale,, Nov-Dec 1969,
pp 54-56.
NASA Tr F-13004
ad/aarmautics
aug 70

HIF:
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