SCIENTIFIC ABSTRACT MIKHNEVICH, P. A. - MIKHNOV, S. A.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001134120019-9
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: June 14, 2000
• Sequence Number: 19
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

MIKMVICH. P.A., lnzh.
Insuring a timely sw?ply of peat to enterprises of White Russia.
Torf. prom. no.1:34-36 '58. (MIRA 12:12)
l.Sovnarkhoz BSSR.
(White Rusaia-Peat industry)

MIKHNZVICH, P.A., inzh.
Poett industry and transportation of peat In White Russia.
Torf. prom. 36 no.7:24-28 159. (MIRA 13:3)
l.Belorusakly sovnarkhoz.
(White Russia-Peat-Transportation)

mll=VIGH, P.A., inzh.; LIVOUCH, GOG., inzh.
Mochwdzation of peat reloading. Torf prom. 39 no.6:3-4 062.
(MIRA 16:7)
1, Be4dprotorf.
(PesLt machinery)

MIKMVICH, P.G.
Powerful nagaatic defect detectors with smooth cu.-rent regulhticn.
Zav.lab.22 no.7:860-862 156. (MLRA 9:12)
(Kota 19--Analys is) (Testing machines)

1 4 4 t 1 42 a f
oil I il

9(7) SOV/3 2-2 5-7- '6/50
AUTHOR: gikhnevich, F. G.
TITLE: Electron-ionic Control by Magnetic Crack Detectors
(Elektronno-ionnoye upravleniye maCnitnymi defektoakopami)'
PERIODICAL: Zavodskaya laboratoriya, 1959, Vol 25, Nr 7, pp 878-882 (LYSSRI)
kBSTRACT: In order to obtain maximum magnetization of the crack detectors
to be investigated with alternating current the current has to be
disconnected immediately when the amperaEe starts decreasing
(second or fourth quarter of period) or reaches zero. For
this purpose the disconnection of the current has to be 3yn-
chronized which can be brought about by electron-ionic control
of the magnetization process. A scheme of arrangement (Fig
of this kind was worked out and two types of magnetic crack
detectors were designed where the current disconnection takes
place by means of Ilignitrons" controlled by thyratrong, and
the current intensity is regulated by means of an electronic
phase regulator. The functioning of the device is explalned b.;
a diagram; moreovei-, the measuring r6sultq (Table 1) in a
disconnection of the magnetizing current by a maenetic swlt~-~h
Card 1/2 and qn llignitr-,n" iyi'.tch on the crack detector are given as

Electron-ionic Control t~- Maornetic Crack Detectors
SOV/3 2- 27; -7 - 3 6/50
wpll Ps rrreri,;uring rosults- of thr- voltaip -f tli~
field an the sample -virface during u s i ng
various ;:f lmlfj~s-rlo(13 (Table). The
tained tJicw (Fie ?) that in (!l-3ctror.-jnrj(-. ccintrol ~.y m,,iCr.~Ai,~
zrack detectors mi,,:netizatlori can take -Iqce with a Current
in sinusoidal form (-,r m~-re cooplicated fcr,,n; hcwever, t1.-?
existine equations for the detenriinatior. cf tht! voltact,
tensity of the maenetic field have to be ccrrected. Ph,?re
are 4 figures, 2 tableq, and I Soviet reference.
Card 212

34949
3/19-3/62/occ/3c, i/oc Woo
koo A004/A!O:
AUTPOR: NTikhnf--.,1ch, P. 7,.
TTTLE: 7r, 1O(,r,G (LME 'OGGC) and ~7(,
crack detectors
P:T,TODTCAL: Byulleten' tekhniko-ekononicheskoy informat-sil, n-). :, Ir".-I
T -_- 7 : The aijthor describer, the new mul-tipur-,,ose ',Y-~DE
mag,netin crack detectors, the former being Intended for checking me(liilr~ an-~
large-size components, while the latter Is to be used for parts of s7al'
medium size. The electron-Ion control of the crack detectors In effectf~d by the
magnetic powder method and ensures a high stability of component magnetiz!ng; a
straggling in mVnetization degree of components Is practically absent. 7-.P
constant magnetic field voltage in the WDE 25GO electromagnet and In the ',.7v7jE
10000 sclenotd for longitudinal magnetizing can be steplessly regulated from
0 - Y'O oersted. The hydraulic system of the crack detectors ensure:; the
spraying of the parts with a magnetic suspension and its continuous agitation to
prevent the magnetic powder from settling on the bath bottom. The following
technical data of the crack detectors are given:
Card 1/3

The 10COO (UNME 10000) ...
AOO VA' 7,
Crack Jptictor,~
Maximum dimensions of parts being checked, mm;
diameter
length with attachment
length without attacNment
Input current voltage, v
Electric motors:
TyPeAO,'--on-4 (ACL-011-4), pieces
power-, w
Type A 3. ~ -I 1 -11 (AOL-11-4). -Iecess
power, w
Type A 0,1-12-4 (AOL-12-4), pieces
power, w
PC A0,1 -22-11 (AOL-22-4), pieces
T
Y
power, w
U?C17 10(1(X IME "I
up to 1'COX ?
up to
up to 1,6rc)
I
5c, 5C
Card 21/3

The' 111)000 (U?4r)E 10coo) ...
mah'P continued:
(Ivorrill (I Imons, Ions, mm:
I (I th
height, without instrument panel
Weight, kg
A(jo4/A"--:
There Is I figure.
Card 3/3

MINITWICH, F.G.
Selecting the typp of current for --agiletic
Zav. lab. 30 no.11:1355-1357 164 ( I .8t1

NEWIVICH- V.B.-: LIKOV. H.L.. kandidat tokhnichaskikh nauk, redaktor;
SM(SHYALOV, Ta.A., Ins),aner, rodaktor; RUDENSKIT, Ta.T., tokhnl-
cheekly redaktor
[Acparience of a turner and repairman] Opyt tokaria-remontntim.
Kiev. Goo. nauchno-tel-hn, izd-vo mashinostroitallnot lit-qj Ukrain-
skoe otdolenie, 1954. 51 p. (MM 8:7)
(Lathes)

Hnafirevicut V. V.
MSRAWsica - Xlectric Discharge
Dee 52
*bqWed D:Loch&rP In & V4PetIc Field With & 3*01al Configuration of Discharg Gap.4
E. M. Reykbrjd*l, A. V. CheMshevskiyt V. V. Mikhawlcbp I. A. Vasillym
'Zhur Takh FIz:Ud* Vol 22, no 12,, pp 1945-1965
rLectrons wOr's NubJGcted to a""" tau*Ous action Of DonhoWgenwus also and axially
SYMMStriC magnetic fields. External magnetic field affecu Potential of Ignition.
00011loaTuPhic observations revealed P~riodic and chaotic oscillations in the discharge.
ThS Mah0dam of discharge at lov pressure is discussed. Received 16 Jul 52
PA 240T100

RNYKHM=', A-N-; CHUMMY. A.Y.; HIKMVIGH, W.V.; USIL'YETA. I.A.
Mechanism of discharge in a magnetic ionized manometer. Vest.kosk.un. 8
no.8:87-100 Ag '53. (KI-RA 6: 11)
1. Fistcheskly faltulltet.
(Ileotric discharges through Cases) (Manometer)

Name MDaUEMCH, V.
Title Candidate of Physical and Mathematical Sciences
R ka In an article entitled "An Automistic Laboratory in Outer Space"
V. Mikhnevich describes Sputnik II as the last stage of the rocket.
The nose cone contain instruments far the study of solar radiation
in the short-vave ultra-violet and X-ray ban" of the spectrum, a
spherical container with radio trains-Itters,, electric batteries to
paver them,, a heat regulator and instruments recording temperature
fluctuations and other conditions. The hermetie2Uy sealed chamber
fbr the experimenta3 dog in fixed on the same rr=L-slike structure.
The instruments for the study of coadd radiation are housed in the
third stage of the rocket. The information traundtted by the satellite
wil.1 be of great scientific value in pbysics, astropbysics and geopbysics
Preliminary processing of the data coIlected from the instruments
recording cosmic radiation has clearly demonstrated the dependence of
the nwd)er of particles of cosmic radiation on the geo-megnetic latitude.
The instruments housed in the air-tight chamber have reported the
reactions of a Living organism to weightlessness.
Source H: Krasnaya Zvezda, No. 268,, 14 November 1957, P- 3, c. 1-6

t
AUTHORS: Mikhaevich, V. V. and Khvostikov, I. A. 49-11-10/12
TITLE: Study of the Upper Layers of the Atmosphere.
(Izueheniye vysokikh sloyev atmosfery).
PERIODICAL: Izvestiya Akademii Nauk SSSR, Beriya Geofizicheskaya,
1957, No.11, pp. 1393-1409 (USSR)
ABSTRACT: Review of pre-war and post-war work in this field. A
certain amount of information is given on apparatus used
in Soviet rockets for exploration of the upper atmosphere,
however, some of this information was published earlier.
Fig.4, p.1401, gives a diagrammatic drawing of a
meteorological rocket which is equipped with small size
thermal pressure gauges. More detailed information on
rocket investigations of the upper atmosphere for
altitudes up to 80 km was published in a earlier paper
b Alekseyev, F. P. et alii (Meteorology and Hydrology,
1457, No.6) and also in a paper by B. A. Mirtov, (Uspekhi
Fiz. Nauk, 1957, September). The results of rocket
investigations are given in a series of tables which
contain American as well as Soviet results. Recent trends
in investigating the structure and properties of the upper
layers of the atmosphere are summarised very briefly in
Card 1/2 the last paragraph, quoting Soviet as well as American

LIN, B.S.. !4IKHNEVICH,, V. V. , RERNSY, A. I.,
ANU DA14
3HftD1COVSKIY,'fe-. -G.- 53-lb-,.4/A
TITLE The Problem of Measuring Pressure and D(ins1tv nf tha Tjjc-*-3
Layers of the Atmosphere by Meanr ct an ArtV11--1a: Zarlh 8&-~*Lxitr.
(Zadacha izmareniya davlenlyk i plotnr~nti v-
atmoofery a pomoahchly-- 1tkU38',veAno9C1 .3;,utr,.k,i z,-m',,
Russian)
PERIODICAL Uspekhi Piz. Nauk `957, Vol 63, Nr 1b, pp 205-225 OSSR)
ABSTRACT By the instrument for the measuring of pressure and density
the authors here understand a "manometer" of any suitable
type (e.g. an ionliation manometer or an omegotrou).
First the authors discuss the various models of the upper
atmosphere. According to the authors the models MITRA and
NICOLST are the nearest approach to reality. A table gives
values of concentration and prebe'une which corr98pond
to various models of the atmosphere. For further pre-,19a
determination of these data tests with rokea and artificial
satellites are quitable. In inve8tigatlons of this kini
various problems arise with regard to the interaction of
a rapidly flying body and a diluted gas. 7he authors here
study so"e of these problems. First the authors dJg-,,sa
the currents of particles, the momenta and the energiet!-
CAD 1/5 for the case of a homogeneoue gas. From 200 icm upward

The Problem of Measuring Pressure and Density of the
Layers of the Atmosphere by Means of an Artificial
Urth Satellite. 53-'b-.
the interaction between a b-;dy moving with a ep7eed Cl
some km/sec and the atmosphere will sonform to the laws
of a free molecular flow. Some preliminary works on this
problem are cited. The behavior of s surfacq is h"ro
calculated which moves with a speed U with r-49pect to the
earth. The energy transmitted by "his surface Is also
calculated. The oscIllation energy Is not calculated
here.
The presure of the flow of & homoganeoua gaa: The surface
1f mentioned above is considered as a plate impermeable
to particles. The total pressure acting on this plate is
calculated. From the corresponding formula the following
may be concluded: At a speed of the satellite of ~8 km/9-
an average molecular weight of the air of-, 20, and at
specular reflection of the molecules (f - 0), the frontal
presure on the surface of the satellite is p , 102 p,
which means that it exceeds the pressure in the free
atmosphere by two orders of maenitude. 7he tangential
stress on the lateral plane surface of the moving body
will amount to zero in the case of specular reflection.
CM 2/5

The Problem of Mensurtne Pressure and Density al ',he
High Layers of the Atmosphere by Means of an krtlfic'al
Earth Satellil-9. 53-1b-14/3.8
Accommcdation c&n be introduced: Like --n the (f ga~3
dynamics, it ejCW4,lg r, #1 toatperpit~;rr- of thp emr,
pregressing povtr was con3umed by Its ':)eirg heated.
During interact'lon with tha screer, the energy car --ewly
distribute over the dogre&s of freedom. Part af the
energy of the progregeive movement of the molasuies c&r
transform 1ts9lf Jrto revolutJoD energy and o,)G4'1,1atJon
energy. The measurements of the coefficients of acoommoda-
tion indicate the following: This ccefficiont depends -n
the kind of gas, on the temperature of the gas, on the
temperatire and the form of the surface and cn the p.resence
of admixtures. The accommodation coefficiects of the
degrees of freedom of the progressive mot'-on and the frpe-
dom degrees o1' rotation are alnios,~ equal.
The equilibrlLm, pzesaure in the cavity of the manometer:
The cons�derati~~n of the properties cf the free mclecular
flow carried out here permits the eatablij)--men* of F%-
CARD 3/5 relation between the pressure and the number -f par--ic,19,3

14
Q
The Problem of measuring rressura and Denei' ' of* ttit.
High Layers of the Atricuphore `t,~, Mians Of aa A!-tif'cJe---
Zart~
in the unit of rolume irA the or-witj of 4.he manom-itor
and the corresponding ;arametors 3f the aurra_ni*_:-.g
me41uz. The authors hare caloulate the moot 3imple --ar.-:
The cavity of the manometer le oonnAoted with t~e &I-
moophare by a diaphragc with the rndiu-; r. The r,~,_rdl -
of the manometer tre ratht)r iiff'.cult to InterprP. 7
V . If
a rather -1 ang 4.,)be I g plaot? I between the oa--i ty of th-;~
manometer ani oatslde atmosphere, ~b- pressure lviWr
the manometer m,.Ist rl,ie. SomethinE is alF,-) seAd abo.~'
the tiMa C3nqt&nt Of the mannmeter; -iviier thp test
conditio,i8 n3sumed h9re 1, Is of a m,%gnitule of 2.IC-11 ser-
Some problems corineoted -vlt~ thti meaeuremjnf, ~)f
The authrra here ahcrt1,- -119~uss the I,oll,wint; p~ b':-fms:
ionization by Impact, "dissociation by impact", t~ie
separation of gag, the electrin charge of the satellite,
the knocking out o! atoms from the a-irfaia of the satel-
lite, the natural ionization of the sttmosp~ere, photoemis-
sion. Finally the apparatus is discuBRed on the basio if
a. drawing. Along the axis of a oyliadrl,jal latti,3e & thin
CARD 4/5

53-1b-14/1.8
The Problem of Measuring Pressure and Density of the
High Layers of the Atmosphere by Means of an Irtificial
Sarth Satellite.
3
ASSOCIATION:
PRESSUND BY:
SUBMITTED:
AVAILABLE:
vire is stretched which serves as ion oollector. Outside
the lattice a cathode with a straight channel is fixed
parallel to the collector.
(10 illustrhtions and 4 tables)
not given.
LibrarX of Congress.
COD 5/5

AU'rHORs UMNEV IC11, V_~~ 53-lb-13/18

ITLE i -
Measuring Pressure in the U,per Atm~s;)hero.
zwurei.i./e
davleniya v verk~;ney atmosfere, Russian'
PERIODICAL: Uspekhi Fiz. ',auk, 1)51, V-,l 63, Nr 1L;, pp 204
ABS-"RACTs In the case of the experiments carried out with ro7kets in the
U.S.A. the rocket serves not only as a mean3 of trarjport but
also as a measuring device which carries out measurements in the
atmosphere, I- th,,~ Institiite for Applied of the Academy
of Science of the U.3.3.1t. the rocket is used only a3 a means of
transT-ort for the a;)paratus when studying the str--ctural para-
meters of the upper atmosphere. A container with the apparatus
is trans,~orted up to a certain hei--ht in a projecting device
inside the rocket '2his container is then ejected in a certain
altitude and continues moving by its own inertia. lie soon as the
container is ejected from the rocket, the measurinp, apparatus
is SWitched on, and measurements of atmospheric conditions
beGin. A parachute opens aut,.)matically and tYe (_.ntainer lands,
the entire meanuring apparatua reLlaining undama(;o(i. fly this method
the disturbing influence exercised by the rocket on measurements
is eliminated to a considerable extent. 2he present work describes
the apparatus and the measurinC results obtaired ir, the upper
atmospheric strata (50 - 100 kin) by means of the non-stabilized
Card 1/4 container.

Measuring Pressure in the Upper Atmosphere. 53-lb-13/18
The Apparatusi Because of the iifficult conditioLa ;revailing
in the rockets, the author used two types olf Laanometerss a
magnetio diacharl-e manometer and a thermal iianometer. By means
of the magnetic electrically --.rCed m&nome.ei-3 iressure in the
-2 - - 5 - -
interval of " .10 1.10 rrr was neasi,r,-I, u~r means of
the thermal manometer ;)re33k:--e was -leasurt,11 i , tl~e interval of
8.10- 5.10-' torr. Phe i.~annor in wl,icf tlie manowetero are
mounted in the container is discusoed. The part of the
container coritains measur4.i,~ devires, a ''.c-ecorder. cl-)cks,
the automatic, and the electrical feedi-n.- his 1cwer
part is hermetically closed, ai,d __LI`i,-I6 the e-- tire iuratic:,
of the experl::ient, normal pressure Is nn, t nqd. Prosqi:res are
registered by photo~-rnphin,, the recordin s ~,f the inensurin6
devices every 1 3 - 1
Results:
Pressures Me author here di3,~_Lj3es t*-,c, r-~x~'3 c,btained fron
two series of measurement3 ~ irriei ,ut In t-c I art -,f
Russia in July, Auguat, and Joitei.il-j. Ocricat The
containers with the apparatus viore laurche,l layrr . in eac'. con-
tainer there were two thermal manometers -.r-d -vD ma(3-ie'ic electric
discharCe manometers. rhe resi:lt3 nltai.-.ed -eas7iri!.t; pres!jures
Card 2/4 in the various containers arc. sno-un, in for-. !ia~;rans.

Measuring Pressure in the Upper Atmosphere. 5 3 - _' t -_'! 3) A 8
Measuring results differ by Lot nore than double their &nount
with respect to differant ccntalnera. I:.11eaeurinR seriesi
Measurements were carried out in the mornine. The apparatu3 was
fitted both in the contalzier and in the rocket. The head of the
rocket contained only the thermal man=eters. The results obtained
by measuring pressure In the container and Jn the ro,-.k4t agree
with each other within the limits of measuring errors. The average
values of pressures measured in the experJmental series I and II
agree with one another. The average quadratic error when letermin-
Ing pressure amount's to 10 ~*. A table and two diagrims show the
data obtained on the occasion of rocket tests carried out in the
U.S.A., An analysis of the data obtained shows the followingi
Up to a height of 85 km the pressure values obtained by the con-
tainer and by the rocket agree with eaih other. At heights of
moke than 85 km pressure values obtained by means of the container
are lower than those obtained by the rocket.
Temperaturet The author did not carry out any direct temperature
measurements in connection w-Itb his experiments. The temperature
of the atmosphere was determined from the pressure determined an tte
Card 3/4 occasion of the rocket tests f7om the barometric altitide formula.

It H /v L V 1 0, 4/L), 0 ,
29(2) ~. 7- PHL99 I BOOKmawITATION SOV/2894
Akademiya nailk SM
Iskusstvennrye sputniki zemlt. vyp. 2: Fbzulltaty nauchnykh issledovaniy,
poluchennyye pri pomoshchi tretlyego isakusstvennogo sputnik& zemli
(Artificial Sexth Satellites. K4% 2: Peealts of Scientific Studies
Obtained by the Third Earth OLtellite) Moscow, Izd-vo AN SSSR, 1958.
82 P- 3,500 copies printed.
Ed.: L. V. Kurnosova; Ed. of Publishing Souse: D. M. Alekseyev; Tech. Ed.:
YU. V. rqlina.
PURP039: This work is intended for geophysicists., meteorologists, and other
scientific and technical personnel engsged in space exploration and research.
COVERAGE: This collection of articles containscertain of the scientific find-
ings recorded by the third Soviet space satellite. Much corruborating
data from other rocket and satellite investigations are included. The
articles axe based on papers origin&lly read at the Fifth Assembly of the
Card 1/4

Artificial Earth Satellites (Cont.) 30V/2894
of the Special IGY Committee held in Moscov in August, 1958. Individual
articles discuss the ionic composition and density of the atmosphere, the
thermodynamic parameters of the atiatosphere,, and questions dealing with
the motion of the satellite. 11eferences accompany each article.
TAME OF CONTEM-.
Sedov, L. 1. Dynamic Effects in the Motion of Artificial Earth Satellites 3
Shvidkovskiy, Ye.G. Some Fesults in Measuring the Thermodynamic Para-
meters of the Stratosphere by Means of Meteorologic Rockets 10
Kirtov., B.A. Perturbations in a Gasecus Medium Caused by the Flight of
the Satellite 17
Mikhnevich. V.V. Preliminary Hasults in Determdning the Density of the
-Atmosphere Above 100 kn ?6
Istomin, V.G. Studying the ionic Composition of the Earth's Atmosphere
by Means of Rockets and Satellites 32
Card 2/4

Artificial Earth Satellites (Cont. ) SOV/2894
Krasovskly, V.I. Soviet Research of the Ionosphere by Keane of Rockets
and Artificial Earth Ektallitee 36
Dolginov, S-Sh., L.N. Zhuzgov, and N.V. Pushkov. Preliminary Fbport
on Geomagnetic Heasurementeon the Third Soviet Artificial Earth Satellite 30
Xbmissarov, O.D., T.N. Nazamy, L.N. Neagodov, S.M. Foloskov, and L.Z. Rusa-
kova. Studies of Micrometeorites by Rockets and Satellites 54
Krasovskiy, V.I., Yu.M. Kushnir, G.A. Bordovskiy, G.F. Zakharov, and Ye-M. 59
Svetlltskiy. Detection of Corpuscles by 1be -Third Artificial FArth Satellite
Vernov', S.N., P.V. Vakulov, Ye.V. Gorchakov, Yu.I. Logachev, and A.Ye.
Chudakov. Study of the Soft Component of Cosmic Bays Beyond
Atmospheric Limits 61
Kurnosova, L.V., L.A. Razorenov, and M.I. Ftadkin. Heavy Nuclei in
Primry Cosmic Radiation 70
card 3/4

Artificial Earth Satellites (Coat.) SOV/2894
VaTilov, V.S., A.P. IAndswan, and V.K. Subashiyev- Solar Batteries 75
Isakovich, K.I. and N. A. Roy. Acoustical Vlethod of Veasuzing the
Mechanical Parameters of Veteorites 81
AVAnABIZ: Library of Congress
Mm/fal
12-18/59
Card 4/4

26-5a-r-lx/',7
AUTHOR: Mikhnevich V.V , -,andidate of Physico-Mathematical 3ciences
TITLE: 3ame Results of InvestigatiQns -)f the Upper Atmospheie (Ne-
kotoryye rezul'tatj issledovaniy verkhney atmosfery)
PERIODICAL: Priroda, 1955, Nr 1, PP 71-72 (USSR)
ABSTRACT: Soviet methods and devices for the inve3tigaticn of the
upper atmosphere are ever improvine. In 1949, rockets con-
taining devices with a total weight of 120 to 150 kg were
launched to a vertical height of 110 km. The ceiling reach-
ed by modern geophysical rockets was 212 km in 1957 find
473 km on 21 February 19580ith a total weight of devices
of 1,520 kg. Recent investigations include study of the
ionosphere, solar radiation, motion of meteors, etc, in
addition to the former study of the structure of the atme-
sphere and the intenaity of cosmic radiation. 3pecial ap-
paratuses included: a diapersion interferometer for re-
cording the concentruticn of electrons in diverse regions
of the ionosphere; special sounding devices to determine
the temperature of electrons; a radiofrequency maj6 spectr~-
meter to determine the amount of ions in rarefied Cuses;
Card 1/5 ion "traps" mounted on the outer surface of the roc4et to

26-58-r),-13/57
Some Results of Investigations of the Upper Atmosphere
measure the concentration of positive ions; ionization and
magnetic manometers to record the air pressure; special
piezoelectric transmitting elements to record the energy
and amount of micrometeors; special dynamic electrometers
to measure the tension of the electric field on the outer
surface of the rocket; a spectrometer photographing the
solar spectrum in the shortwave ultraviolet range. Re-
sults of the stabilized vertical rocket launching of 21
February 1958 included the fact that there is no clearly
defined ionospheric layer at a height of 110 to 120 km,
The electron concentration beyond 110 to 120 km at first
decreases insignificantly, and then graduallyluntil It
reaches a height of 250 to 300 km. Over 300 km the electron
concentration decreases slowly. At an altitude of 473 km,
the electron concentration is equal to one million electrons
in a cu cm. This may be explained by an intensive diffusion
of electrons from lower layers of the ionosphere. The ion
amount of the atmospheric air was determined up to d height
of 206 km. Air samples taken by special balloons up to a
height of 120 km disclosed the second Important fact ob-
Card 213 tained by rocket investigations: there is no diffusion

26-58-5-13;'5-
Some Results of Investigations of the Upper Atmosphere
separation at an altitude of 100 km. Hits from micropart-
iclee were registered up to an altitude of 500 km. Prea-
sure and density of the upper atmosphere was recorded up
to an altitude of 260 km.
There are 2 Soviet references.
ASSOCIATION: Institut prikladnoy geofiziki AN SSSR j*Yfioscow (Inntitute of
Applied Geo"ics of AS USSR, Mosc(rw)
AVAILABLE: Library of Congress
Card 3/3 1. Upper atmosphere research - USSR 2. Upper
atmosphere - Test results

WKiNEVICH. Vern, kand.fiz.-mat.nauk
.
On thm way Into space. Rabotnitsa 36 no.7:22-23 JI l5il.
O(IFL~' 11:9)
(InternatinnAl Gsnphysical Year, 1951-1?58)

MIXMVICH. V.V.; DARILIN. B.S.; REPIIEV, A.I.; SOKOWV, V.A.
~:M
Results of determining atmospheric-structure parameters by means
of the third Soviet artificial earth satellite. Isk. @put. zem.
no.3:84-97 159. (MIRA 12:12)
(Artificial satellites) (Atmosphere, Uppar--Measurement)

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S/169/62/000/010/062/071
D228/ '307
~0-1 HOR: 1.7.
~IOMC rC3Ult:-, 0- atmosphere ar,6 a 'ace -,csc!arch
by me %.7,.-- o- rocI-.ct_- And satellites in the Soviet
Union c:ii~:in_ -.he 1GY
Llcfera.:-~vuyy ~;Jivxval, Geofizillra, no. '10, '1962, G,
10 "'J';
abstr.x'.: 10646 (,3cofiz. byul.I,'czhduvcd. gcofiz.
kom-t pri 'rcZidiume S."SP., no. 11, 1962, 22-32)
Some result-- o" hi-Ii atmos?hcric -layer a-_L! space
rosearch during the 1GY arc in a gencral form. Research on
structural parameters, t.io ionon-)hcrc, the magnetic field, cosmic
lar emis3ions is mc
raciation, meteorite and Cifferent so n-
tioned. lt is pointe6 out that 175 rockets -wero Afired in the 'kj.;Sjt
during; the IGY, 17 cZ ,:*,-,Cnc . . -fco-:)hyzical and 153 mctcoroIoZ;ic.
'C 1-1~ o .
~-)hcrical (space orientcc!) ;,,nc! cvclindrical containers, carrying
tLic intricate complex of-' gco.)hy~ic,-.1 cquipment, were employed on the
rock4ts. The firin[;s of 'J'ovict -atcLlites and space rockets, and
C; ard 1/2

..;,/169,/62/006/010/062/071
Some rc~Gults Of UP..)Cr J223J/D307
t',-Lc maiTL ,cophysical jy 04,
J.
c-all-acrated: Of
the magactic -lield 0-17 -L- LI-1c, ":~Lc Mooll; the i-,,Vcst4., a-,io-,l of
distant rc~;ions of -L'-.c fron tau vieinoi-at of t i c --' r
electron concenzl'atic)-l' "::Iat Of t:-Leir ionic composition;
measurc-nents of t:-Ic C., l' ~;arcous mediun to a distancc of
500 in; the c,. L.,~L frequency of collisions ~dth micro-
netcoritco; and al~;o of heavy nucle-4. in the conposi-
tion of 'irimary COs-.-uLc
L .abstracter's note: '~om,)lclkc
Card 2/2

MIXHNEVIGHP V.V.
Atmospheric density variations at altitudea ribove 2ff, km.
lak.sput.Zem. no.17131-41 163. fMIRA 1.,,0)
(Atmosphere, Upper-Density)

L 2988-66 - F5S-2f/EWT(l_)/FGC/EdA(h)- - r.S/Gl-----
ACCHSSION NR* Ar5023554 UR/0000/65/000/000/0023/0029
AUTHOR: Hikhd~ ~ch ~V.V.
TITLE: Density and temperature of the atmosphere from measurements made in 1963
with ait automatic high-attitude geophysical station
SOURCSt Voesgyuzn!ya konferentsLya-po fizike koomicheskogo p ostranstva. _1138
1965. Iveledovenlys koemichaskogo prostranstva (Space research); trudy konferentaii.
Ixd-vo Hauka, 1965, 23-29
TOPIC TAGS: atmospheric densityY"/atmospher1c temperature, meteorological rocket.
I geophysical research station, upper atmosphere
ABSTRAM Rockete~/Contalning automatic high-altitude geophysical stations were
launched on 6 and 18'June 1963 to study the properties of the upper atmosphere
(in excess of 500 k~). This equipment Included Ionization and magnetic discharge
manometers and other instr , utro for deterAining the density. pressure, Wd tempera-
'~tjjre of tij-_ &tn4voeve. The equipment was hermetically sealed, and there were no obstrdc-
tione in the field of view of the Ionization manometers. The Instruments were
stabilized with respect to the sun during the flight, and measurements wow made
during the ascentand descent of the rockets. Tfie results confirmed previous dataj
Cmd 1/3

L 2988-66
JACCESS1011 14R1 ATS023554
the density of the atmosphere varies considerably above 200 km. The observed
variation in the atmospheric density (see Fig. I of the Enclosure) is caused both
1
by the reduction In.solar activity and by the diurnal effect. Measurements of the
laltLtude of the homogeneous atmosphere and the atmospheric temperature show a
reduction in temperature at altitudes of 0-165 and %265 km, and an'tocresse In
itemperature at altitudes of %143'aad IQ15 km. Comparison with previoue'dats Indicates
!that thete Is a temperature inversion in the region between 100 and 300 ka. The
author recommends that this temperature Inversion be studloid further. OrLg. art.
has: 6 figures. 1141
1ASSOCIATIONs none
!SUBMITM 029ep63 ENCL.6 01 SUB COW: ESISV
10
.NO REP SOV: 003 OMER: 0 PRESSt
Card Z/3--

L 29&~-66
A025SION MIS AT5023554 ENCLOSUM:
f
'w
-~';% Nw.
31
Fig. 1. Atmospheric density
OL
L IS June L963, middle latitudes of the European section of the USSR,
automatic hL&h-altLtude giophysLcal equipmftt, wamometers; 2 L6 may
L958 - third Soviet artffictaf,~earth satellitso manometers.
CewdC313

L 547-404rl- 113-2/0M1 )/FCC/aC(t )/EWA (h) - - -PD--4/Pq-4/P&*4/0eb/P1-4 (MI
ACCESSION SR: 156T3. UR/0293/65/003/003/Ok5T/0468
AP50
551-510.3
AUTHOA-: Mikhoevich-1 V., Golubev,_Ye. N.; ParfianovichjL Yu. N. 3
TITLE: Prellininary results of determining particle concentration and stmotopheric--
density on 18 June-1963
SOURCE: Koeiiicheskiye koledovaniya, v.*3, no. .3, 1965, 45T-468
~TOPIC.TAGS. atmospheric density,. satellite -mission iLnalysis, geophysical, catellite.
solar activity, atmcs~heric pafticle con"ntration. quiet elm, ultraviolet
radiation
ABSTRACT.,. Analynes of the results am presented for manometer determinaticne of
atmospheric~densities' 'and pexticle donceutrations at altitudes between 120 and
--360-km made on 18-Jund 19�63- The vehicle-used-was a high-altitude automatic geo-
~1 physical station (VGAII),Vvhich was 1 m in.diameters weighed about 360 kg, and
carried 5 (2 Ionization and 3 electric-discharge magnetic) manometers in addition to'--
amplifying apparatus.l~ The arrangement of the mancmeters In the satellite in shown
in Fig. 1 Of L the Enclosure. A description is_ given of the satellite's trajectory
and operation. The solar radio-emission flux at the time of flight (accotding to

AMR
_A4740.4
ACCESSION Nft*. AF5on673
the Mora Observator Canada.) wash 82-10-22 -w-rs72 cps-1. kanometer readings were
interpt etIeii -using the method describbd by A. I. Ivanovskly and A. I.*Repnev (Tr.
TsertraJ.. Aerol-'Ob6itrv., no.-56, 1964). -An analysis of the dependence ofthe
formulim; used to Aetvitrmlne particle concentrations and densities on temperature
showed -that the fas 't!er the -instruments moved, the more accurate the readings
became.. Under. the conditions of this experiment, the effect of manometer qensi-
tivity on- the' readingo .is explained and analyzed. The error in the determination
of the Orientation angle between theapparatus and the vector of the flux velocity.
was about . 301. Figu.'.2.and 3 show graphically the results obtained. It vus found
that at' an. altitude 6f over -200 km, atmospheric density dWni~hefir with diminution
i&Uvity-bi -,belm-this-altitude--the~-effect-of- -solcr activi -Y is
W the
Or as4
intionoeqiWtitial.' 1g; aft. bus 10 figures; 3 tables, and 16 formui
ASSOCIATIOJFJ~ 'none;
StMMITTIM 10jun64 EMM '02 SUB WDE: 10,, 5V
Ito 1M1F.;S0V11! COB OTWI W6 MD PMS: 4030

1~-

-L 347h5:!Mk- zw- (1)/F00 GWAiS-2
h0ffI0621
-Aa'RW--AF6025229 SOURCE CODEtUR/0384/66/000/001d
AUTHORs Ukhnovich, V. V.(Candidato or physicomathematical acionces)
O,N: none
TITU!'.: Summary of recent upper atmosphere research
SOURCC: Zemlya I vsolonnaya, no* 1, 1966, 17-21
TOPIC TAGS: uppor atwophero, atmospheric tomly,)rature, atmosphoric flonsity, man-
ometer, mass spectronstry, nitrogon
ABS7,,ZACT: Measurements of 6 and 18 June 1963 revealed that the temperature
of the atmoophere above 100 km does not increzatse monotonically; Instead#
..there are maxima and minima. Of particular interest are the results of
mass-spectromoter investigations of nitrogen, since in this case no
assumptions concerning the composition of atmospheric gas are made vhen
determining temperature. It was found that at heights of about 180 and
270 1a3 there is a minimum and at heights of about 160 and 220 km there
is a maximum. Such a variation of temperature with two maxima and minima
in the region from 100 to 300 Ica was recorded on 18 and 6 June 1963 with
manometers* On IS June the temperature minir-n was situated at heights
of about 165 and 265 kmj the mwdmum. was at about 145 and 215 kn. On 21
L-rd

L A745-66
ACC NR: AF6025229
reoruary and 27 August 1958 the temperature minimum was at about 175 and
185 'ru-1. '.Wcima and mini-ma also are observed frequently in the curve of
the change of temperature and the height of the honogeneou3 atmosphere
computed from the deceleration of satellites. Obaervations of four satel-
lites revealed that in the region of approximately 220 1