SCIENTIFIC ABSTRACT MERZHANOV, A. G. - MERZHEYEVSKAYA, O. I.

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December 31, 1967
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SCIENTIFIC ABSTRACT
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A. G. fns of heat tranSfer in t,,p ,,eat --'Y-.rjj(-,rior-l tr lip-roble -s Trealsfe", report subraitted for 2nd Ail-Uniol "'If on Heat ' Mas jilay 1964. inst of C,,Iemical Physics; 1)~S USSR' I ACCESSION NR: AP4043201 S/0207/64/000/003/0118/0125 AUTHORS: Barzy*kin,,V. V. (Hoscow); Gontkovskaya, V. T. (Moscow); Yarzhanov" A.-G. (Moscow); Khudyayev, S. I. (Moscow) TITIZ: Nonstationary theory of thermal explosion SOURCE: Zhurnal prikladnoy makhaniki i tekhnichaskoy fizdki, no. 3, 1964, 2-18-125 TOPIC TAGS: thermal explosion, h eat transfer, Newtonian heat exchange,, thermophysics, approximate formula ABSTRACT: The authors use an electronj~ computer to analyze and solve a system of partial differential equations for thermal explo3ion for,'a reaction of zeroth and first order with conductive heat transmission in the reaction zone and Now- tonia:.i heat exchange. on the boundary. They -.aoalyzo____ ao 0 and 21 7V W 0XP + + i-+Po (P (10 OXP T+ 0 a at, 4 at P (F Q6k*1 exp - In- . L 4 CPR 0 Q8,2k* GXP a -r CPRTQ" (2) -07VT (- Qu Card '1/2. ACCESSION NR: A?4041201 'where 9 is heating, 7-is tire, gis a coordinate, (5 is the criterion of Grank- Kamenetskiy, n = 0,1 and 2 respectively for plane-parallel, cylindrical, and spherical containers, ~ is the depth of transformation. The dimensionless var- iables are: T(x,,t) - temperature in the reaction region, To - temperature of the ambient medium, Q - thermal effect of the reaction, k. - pre-exponent, E activa- ,tion energy, A - coefficient of heat conductivity, c - specific thermal capacity, P - density, R - universal gas constant, r - radius of the container (for plans- parallel - half of the thickness). The authors refine the determination of the basic characteristics of thermal explosion. They present the results in the form of approximate formulas relating the characteristics of thermal explosion with all the parameters of the problem in a wide range of variation. A criterion is given for applicability of the equation averaged over the region for computing the period of induction in the case Pf conductive heat transmission in the reaction region, and a method for averaging the system of equations for thermal explosion is proposed. Orig. art. has, 5 figuresp 6 tables, and 9 formulas. ASSOCIATION: none SUBMITTEDs 23Jan64 ENCL: 00 SUB CODE- TD NO R17 SOVt 008 OTHERs Cat-d 00~ 2 V::To I =-il~ ~~j 4 N "I V PT:' j, /2 4 ~P J~T-~,j /JW /TATD/rdl S/0()6Z/64/0W/008/1509A: 1ujVi:xN)10F 14RI IP401,41705 511 ;i urlibut G. -Filonanko A K J! T ITLE -Thleory of reaction e r g i rae r. in f I ames in the combustion.ofl n no volatile condelised systens SO=E: -All SSSR.' Izvestlya' -,,rjr:Lya ki 8, 10,64 1509 1511 3 Amicheskaya, no. TOPIC T1 ruSi combust.-ILon- mmloalve pyroyalline solid propollant 1 AB-T1W"0T:- . The 1epp"t1i of the darl': -ne- (x and as ng rate -preflama zo tho ma buxni detorl-Arled by ibustion. of xilino P10 0 _t1 CM J11 diOJWtar. -3-4 cm ;uz- r e Coll yro. TIM long) ubdch were coniproaced to de Mities -Q~ing from-0.8 to 1*5 g/cm The nhtswera conducted at 20- 'O.at Ti-e-zsurn -in -a conatartt preasure bomb ezverim EV, axppmr m"rintal romil 0 (6 0 Figi. !-and 2 oV fi led with 11itrogen. 6 qlUation of t 11;-,) t shoued that -the Pxperirnental:dalua can be-torr lated by the- proilotmly- dorived thaoi;ctic.al . relau 1.p xf at .FRIh -65 I/E 1 T, 1.6033 00) S/0076/64/0381011/2640.1,2641 ACCLSSION N R., AP4049606 AUTUOR.- Barzy*kin V.- V. ~(Moscow) Iforzhanov, A,11G. ('Ho s c 01.1 und r c n TITLE S tudy of thermal explosion of conda-ftsed- gyn tems~ a 0 d i t;i.on aof-jow heat trannfer from tha Gurroun Iding medi-tim souRce z1iurnal*..fizichesk_oy -1chimii, v. 38,- no, 11 26~40-72647 re, induction peri-od,. ~etryi-, TURIC TAGS: explosion critical temperatu dinktroxye thylami ne ABSTRACT:1 A~method for- de termining from small samples. I- 5-p, the critical temperature and tha induction.periods o f n ew exp.losiVes has been d dve I o p e d-. Previous 1 Ab o ra to ry !methods _,fo_r,determinin~ the, qritiedA parpmeters -from small. samples _.-ising a- directly the-kmostated reacti~tn_-vessel gave inaccurate results. -The method devplo,,,ed use!; very 1~ .)w, hea t-transfer coeffi. .cients on the or der'of I.0-3kcal/cin2 sec~grpd._ -The reaction vez sel is cquipped~with~two jackets.' Water from a, thermostat is-circ'ulated through the outer jacket, while the is'either evacuated or' filled-.withair, The temperature A.CCESSION NR: AP4042212 S/0020/64/157/002/0412/0415 AUTHORt MakaLmov, E. I.; Merzhanov, A. G. TITLEt A model of burning of nonvolatile explosives SOURCEt AN SSSR. Doklady*, v. 157, no. 2, 1964, 412-415 TOPIC TAGS: explosive, nonvolatile explosive, liquid explosive, solid explosive, theoretical burning model. combustion, propellant ABSTRACT: Parr and Crawford9s theory of burning of liquid explosi-res through the formation of foam in the condensed reaction zone (J. Phys. Coll. Chem., 54, no. 6, 1950, 927) has been further developed by theoretically treating the problem of the mechanism of dispersion during the burning of nonvolatile liquid and solid explosives. A i i jaingle-stage model of the burning process is considered which takes into account reactions-in the liquid phase with a large expansion ~in volume caused by the formation of foam, which is transformed into !an aerosol. The reaction in the gaseous phase, the dissolution of ,the gaseous reaction products in the liquid phase, and the heat !ACCESSION NR AP4042212 losses from the reaction zone are neglected. The heat capacity is assumed to be constant. The equation of state for an ideal gas is applied to the pressure in the foam bubbles 'and the aerosol. An approximate solution of the initial system of equations derived for the burning process with a large expansion in volume was obtained by ,using Zeldovich and Frank-Kamenskiy's assumptien that the convective heat transfer in the reaction zone may be neglected. Numerical values of various parameters of the burning process were calculated on an electronic computer to verify the approximation. The data i .were in fair agreement with the theory. Thus, the proposed model ;may be used for calculating the burnfng velocities of liquid and ,melting, solid explosives. Orig. art. hast 2 figures, I table, and I 1:6 formulas. IASSOCIATION: Institut khimicheakoy fiziki AkademiL nauk SSSR ;(Institute of Chemical Physics, Academy of Sciences SSSR) SUBMITTEDt 23Jan64 ATD PRESS9 3067 ENCL: 00 SUB CODE: WAv FP NO REF SOVt 009 OTHERt 002 Card: 2/2-- 0-5 Df.;, _1_IV$1TdW JIM Filt ~11.7. 14 30 ~Sj 00 2 0 6.4'/ 5- -f:1,0-0 6 14 -.A- G Y a a im6v E -.40,-'Herkhat, iv _'AU Ito r ition- of' exp~kosive p, r ti r'-I e s in - a hot -157-, no. 6 1-4964, 142 7- 14 30 5 OURCIE Ali SSSR. -DoIklnd,"*, V, Ignition$- combust TOPIC T AG 9 explosi've ion, propellant, kolL '~Prorellant ig nition delay :ABSTRACT*., -The ignition of, sphe'rical barium az.~deipdrticlcs produced :by abra,sion of crystals on emery paper was ',studied at-260-1650C in 'vin a s a em, bjf~ containing an-eler-tri,cally heated vertical glass -tube into Y, -par ticla--waa -.-In trodtf6ed -f rom the-, top-~ and ~ prehe a ted air or 'w'-fr-m- the~'-_--6ottom._ -The I hiling -speed-af_ th;-- partic-le could- be ~4 r -c u r r e n i__- a'i r a v For-shorter d _~,,Th a i iti use gn v7 ENCLOSURE: 02 . ,.!' POP, 4044885 R AP ACCESS16i4 N A /go 113 its Is, T 2. Depeladence cr b Fist welu 'XA(its: .,tnerma.L expiosion,. combustion, ignition, combustion tneory, xinetics, reaction kinetics ABSTRACT: A theoretical study has been made of thermal explosion with varying tem- -perature-of the surrounding medium. The parameters ofthermal explosion were cal- culated.for mondmolecular, bimolecular, and autocatalytic reactions. Exact and approximate solutions.were obtained by numerical.integratiohand by pseudoisothermAl approximation, respectively.- A plot of.explosion temperature vs the rate of heating showedl,that.in monomolecular.reactions, the.explosion temperature decreases vith in- of heating to the.critical value'corresponding to static conditions. JIn alyti'~reactio_ on conversion the.explosion e auto at a ns, depending temp rature either tirst nor es eases( and- then decreases or it only increased. Orig. art... has: 2 figur ~21_fdrmtnas -and 5 tables. IPVI ~t.SUB:CODE: TP/ _SUBM DATE: 02ffov64/ :ORId REF:' -oo6/ ATD PREss: Card; L 7703-66 7 SOURCE CODE: AP5096031 UH/040j/65/ 000/001/009310102 AUTHORt: GrIgorlyev, Yu. M. (Moscow); (~oscowh Merzhanov A. G. (mos. COW) ORG:- none, TITLE: Relationships of i gnition of homogenous explosive particles in hot gas SOURCE: Naaichno~-tekhnicheakiye.probleqr goreniya i vzryva, no. 1,1965, 93-102 TOPIC TAGS: combustion, explosion, !xglosive opellant. solid propell ignition pr. ci ABSTRACT: A-theory of thekinetics of decomposition of nonvolatile explosive particles,in a hot gas has been developed on the basis of a simple model which assumeE the action-takes condensed particle the exothermal re place,on-the.surface of the I which~:,doea not unde phase trins formation or change-of size in the pre-explosion r9o ~perbod 'that 'the spherical e losive particle enters a cavity filled.with hot gas, Xp that- he6t transfer insidethe particle takes.place_by conduction and external heat.: _trdnsfer by canduction,and:radlation, an that convective transfer is absent. The, d analysis yielded expressions for the tetaperature profile ih the gas and inside the 'particle, for:-the'tim6 required to heat the'particle, and for the induction period.,._ To verif~f the theoretical relationships,.experiments were made with nitrocellulose- -13YMXylinii powder%articles (50-150 V,particle- sizel in horizontal and verticbl _Oass.tubes. The igaition-temperatures of 50 v particles were 255C in air and 246c Iscro v2 6 E' L 4519--6 /-,/FC-) (QIEWA (c (I RFL ACC N R-. AP5026067 rall/al/wE RM SOURCE CODE: UR/0405/65/00O/0O2/oa62/oo68 At1THPR:: Lisitskiy.-V. la ..(14oscow);.Verzhanov G. (Moscow) ---------- OM none I gaLt -ion f condensed substances by the flow o -SOUNCB: Nauchno-tekhnicheskiye probleaW goreniya vzryva, no. 2, 19651 62-68 TOPIC TAGS:: explosive ignition, ignition theory, ignition delay/pyroxylin no 1, ABSTRACT.- -Previous studies of the ignition of condensed explosives by the flow of hot, - gases have,not accountedfor the heat exchange conditions. Therefore, a new apparatus was designed in which the heat exchange between the explosive and thegas s measured under controlled' condi ti ons xyl Ignition,of Tylindrtcal charges of,pyro i :No. 1,,O.06-4.8:~c 3 bythe fl-ov--o-f-Tiot. m in diameter d and with a,-- density P 1-5 g/cm e atltlie gas temperature or ca n dioxide) was studied gas -s - (6.ir' nitrogen, axgon, rbo gas velocity u = 90-270.cm/sec' Re'= 150-550, and ignition delay To =..250-370C9 an delay was determined as a function of To, the time t3 =~ 15-95 sec The igni -wpperatureLotthe pyroVIinWcharge 'kH 31 and the heat.transfer coefficient a. Mathe- ma:Ucal, treatment the expeximental results within the similitude theory yielded 1/2 UDC: 536.46. d: CC .[A NRj AP5026067 the f6ilowing expression for determining the dimensionless ignition delV time: '%,=0,01602H7-, yhere r RtO2 - T- ' (EIR TO)] exp Q. Herej Is the thermal effect; C, specific heat; E, activation energy; and -in 1. 64. A graphical presentation of the experimental results in dimensionless, coordinates shows that only under the following conditions v. G) ~< -c; (H) < -c~' 't. (0):, does th above,dquation correctly describe the ignition of pyroxylin 1~y -ffot gapes --dnd is prob. ably applicable for o*her condensed systems inwhich the ignition is not accompanied by phase transitions. Orig.~art. has: 5 figures and 4 formulas. SUB CODE4~, MC/SUBN DATE: l8jan65/ ORIG REF: 003/ OTH REF: 005/ ATD PRESS:11M ard 2/2, )/FPF(&)/TIF CZ(k) X-'M(c) V 3 L Wo-& MjT,(1)AA1n(M C NRe. AP5026074, SOURCE CODE: Ult/0406/65/000/002/0108/91- 14 B, i AUTHOW Strunina; A.. G.; Merzhanov A G - Mayofis, Z. MTLE-., Dynamic, thermal explosion conditions. Part 2.. Thermal condition regularities during constant rate cooling elknicheskiye gorenlya i vzryva, no. -114 N hno t 2, 1965, 10 SOURCE: auc 8 p 4: TOPIC TAGS: heat of explosion, cooling rate, thermal explosion, explosion intensity 57 Y 5' ABSTRACT The first part of this paper (Nauchno-tekhnicheakiye problemk goreniya, I vzr%yva, 1965, 1) investigated thermal explosion conditions during the heating of the surrounding medium. The present axticle studies these conditions for the case of coolin The, explosion pattern and -its basic characteristics'are studied. The .-..:derivation, of the approximate solution to the problem, the results of numerical computer integrati -system of equations, and a discussion of the critical heating on of an original rate, pre -explosion heating, and of other pertinent -explosion reaction intensity, pre --parameters describing the. events are given.. The article concludes with, a discussion of the application of the.linear cooling method to the experimental study of the thermal explosion of stronglyself-accelerating reactions. The: authors thank. A., S. Ukolov.-, .5~, V, as for several computations carried out during the: investigation. Orig. art. has: -13 for .5 f* imires, and 3:tables UDC: MiJMM6.48 SUB, CODE., WA.FP.TD SUBM DATE: 23No-v /0RIGREF:0037.~-__ Mo 1; 158~,0_66.. W41 pID/WL, AEF-MAP6064428 SOURCE'COD8: Ilk/0414/65/1 /00 /0636/0040 A. G. ;AUTHOR: Str"a, A. GIffascov); Gontkovskaya, V. T. (Mbscov); MES*oy (Moscow) 'ORG: none ;,TITLE: -Dynamic conditions of thermal'e I osion. 111. Temperature field during' ~'heating and problems of the transition from spontaneous combustion to i *on ~SOURCE: Fizika goreniya i vzryva, no. 3, 1965, 36-40 JOPIC TAGS, chemical explosion, combustion kinetics, temperature distribution ABSTRACT:,, Equations for thermal explosion during heating are numerically solved :withregard.to temperature distribution. The paper is a continuation of previous studies. (A.' P. Merzhanov, A. G. Strunina, Scientific and Technical Problems of Com- ibustion.and Explosion, 19651, 1; A. G. Herzhanovs A. G. Strunina, Z. B. Mayofis, iscientific and3echnical Problems of Combustion and Explosion, 1965, 2) and the no- I.tation is the same as that used in these articles. The problem was solved on a coin- 1puter.- AniLysis of the numerical solution shows that ignition under dynamic heating ~conditions:ls completely analogous to the process under static conditions. The ~7_ ~Card.1/3. UDC!, 536.46+536.48 -15870 66 ACC RR: AP6004428 lbasic parameter in defining the exchange conditions -'is the rate of heating w. ~'Curves are given showing nonstationary temperature profiles for a monomolecular ree-, ~,Iaction at a Biot number of.infinity and various values of w. rour regions are dis-. Itinguished with respect to heating rate: 1. &a y.6j.-or y < ycom. The folloving additional conclusions ar4 ~co icn gnitidn. The i !made: at low . MeN -the zeact!-On m4y beassithned t6 ~be of zero order. a formula previously -ed-by Zelydovich are in some. ;delay times caiculated b~ develon cases about 50%.lower than the acVual values. Therefore,,.this formula cannot alwaY9 cti~c 'be used. The width -of -the -reaction zore under-a normal regime is pra ally in- dependent ~of: the t mperature difference :between the source and-the propellent , Orig. [PV] art.- has: 9- formulas.- --ASSOCIATION. Filial Institute khimicheskoy fiziki All SSSR ~W "(Branch ot., t4e Institute, -for Chemi cal- Physi cs MI assrl) 'T -26, D: Tar,65 EN SUB "CODE: FP SUBMLTTE CL 110: FM V SOV: -003 0 TI IE IIR 0 02' ATD PRESS 2/2 EPA/FP.,k(s'-2/E Po' .3" Acu.-r.:ssiou IIR: A_v5ol,7461 UR/0020/65/i62/005/1115/1118 'AIUTHOR- Maksimo I.; Merzhanov, A. Kolesoy' TITLE: Density -distribution inthe combustion zone of-condensed systems. ISOURCE- All, SSSR. Doklady, v. 1965,1115-1118 162, no. 5$ -TAGS: ,,"(:Lo olid p ITOPIC _T~b!_ 5 ropellant, hexogen, combustion mechanism, condensed, phase reaction -based: -6 !lobed RACT, An,expe_iimntal inethod on x-ray a sorption meai~~trements was dev( - - - =ity rT Tile- at- irface--6f a so prop ant d6-t6tjni&ng t e Iens f4e-_burnin lid ell c 5 atm - sbowe - tbat-the -density c Px~h e MeAhod.:aD lied to hex oinvustion"at 0.5 to A changes considerably with -pressure and that the densit ,profile ~y change is gradila iThe thickness of the Zone in mhich the density-changes,can be, calculated as a func- ..~_ition of the propellant density by means of a Tormula, derived. Motion picture plio- 1tograpby sbowed that foam formed in the.molten propellant layer leads to -aerosol Iformation. foam formation isattributed to the chemica2l, reaction in the liqldd melt rather than to-passage of gases or to -'boiling of Ahe overheated melt. -, The: chemical conversibri Iin the:liquid phase was evaluat ed as 0.15-0.35. Comparing the* Velocity. i of the reaetioa front propagation with the burning: velocity actua32y observed, At oho- Al M 't latter and that-* ved--that- he 16, ar -is -one order of magnitude smaller -than he AMMON NR: :AP5013086 UP,/0020/65/163/001/013310136 ~j AIJIHOrt Bostandzhiyan hanov, A.G.; RMfta7 T! LEM Hy on drodynamic thermal exploai 163, no. 1 1965, 133;..136 1 -SOURCE. AN Doklady v- V'~' F TOPIC TAGS- hyd dynamic -thermal explosion, exothermic reaction, thermal explo- d, laminar flow, nonlinear temperatufe sion,' chemically1nert fluid, visco" flui dependence,, energy dissipation, nonlinear heat source-: ~M_ :ABSTRACT.-- In the resence of an exothermic ..chemical reaction in a system there -P may arise-conditions in which temperature progressively-increases until the so- gy wi shows called thermal explosion takes place. By amalo th the above, the author -off ect- similar to thermal ex I sion may take, place during th that an P 0 e flow of a ~inert Viscou ais illustrated with an- elementary examp chemically- P fluid. Thi le: ble fluid Ithe at& I nary tric. laminar flow of a viscous incompressi -axially symme of- fixe&.density in an inf ini t e1y- long round tube-under the action of a fixed 6- -Theaystemol-equation o m ressure gradiefit, s- f otion-and-heat conductioni on: P tzaking -into accauut energy dissipation, is,presented And, for the particular case i;:qr4 1_3 6--203 -55 ACCBMN NR: AP5018086 of-flulds-with it strong temperature-dependencoof viscosity* reduced to the Fequation dSO I d0 = 0. + uhichIs I-dentir-a 1, -with the ~equation_ of the stationary,theory of thernial cyplosion. (see, e.g.-Frank-Kamenctskiy, D.A. ZhFKh, 13,~no. 61 738, 1939). ThU 9 many of the inferences of this theory may he applied to ~thc case considered here. Proceeding from-this.premise, the author derives formulas-for the calculation of,critical the al losion" in -the preganc c0 Ations ofthe hydrodynamic,- exp of Re numbers At which the flow is laminar. This is illustrated by the.calculation. of such critical conditions for glycerin-at-Re- 500. The differences between.thermal " ex- -olosio n" of chemical and of hydrodynamic origin are- defined. I-lius during the f low of-a-Viscous fluidtftheliberation.of heat ultimately corresponds,to a zero-order. reacfioil" And - the - do-called - I'b~rnout" is absent.- Furthermore the maxirmim in..tea- 1 - sity of cbemicall sources of- heat -is present in the center of the, sy'stem. wherean for mer-hanical sources it is preaent near the surface. As a result, the stationary temperature profile irk the hydrodynamic-problem is:flatter.in the central layers and-steb-per in.tbe surface layers. The overall findings-thus indicate that in the ow cage of a strong -(nonlinear) temperature-dependence of viscosity ing to energy- 77-' t. 93975-66 FVF(m) jaF(n)-2_/T/E?2(Q UTIP(e) AO~ Mg AP6012523,. SOURCE CODE:, UR/0062/661000/003/0422/0429 A. 0. AUTHOR*, Maksimov E1 Crigorlyev, Yu. M.j. Merzhanoy ORG: ~Institute of Chemical Physics Academy_of Sciences SSSR (Institut Winicheskay f iziki AkadeiHi nauk SSSR) TITLE: The rules and mechanism of ammonium percblorate combustion 96 SOURCE: AN SSSR. Izvestiya. Seriya khimiFheskaya, no. I,MK96, 422-429 TOPIC TAGS: ammonium perchlorate, combustion, solid pXopellant ABSTRACT: The thermal decomposition of ammonium perchlorate (AP) is discussed exten- sively in the literature. PA sublimes on hi3ating under high vacuum. Sublimation is ~suppressed with-rising pressure and decomposition with evolution of heat takes place. Burning of PA occurs.only at higher pressures. The purpose of this work.was to vestigate.the nature,of combustion of PA depending on temperature, pressure, particle size, density, and addition of ammonium chloride. Experiments were conducted in a cons t~ant-press,ure bomb under nitrogen. The temperature was maintained by circulation of a thermostated liquid. The rate of combustion was determined photograp Ihically on ~A moving film.- Technical grade- PA was used; results obtained from PA purified by -'recrystallization differed by no more than experimental error (t4%). Samples were obtained by pressing PA which had been ground and graded according to size. Formation LCard 1/4 UDC: 541.126+541.124 .U. CZUU7~uu - rlVTL11714-1~4 nvrkr'~ Idukc) i7YEA UZI fif 144 ZI F?, ..,ACc NR. A_p6ooft96 SOURCE CODE: UR/0076/66/o4o/ow/068/070 AUTHOR; Maksimov, E. I Merzhanov, A. G.;,Shkiro, V. M. ORG:-Branch of the Institute of Chemical Physics.Acalemy of Sciences SSSR (Fild? Instit.uta.khimicheskoy fiziki Akademii nauk SSSR) TITLE: Self-ignition of thermite mixtures SOURCE: Zhurnal fizicheskoy khimii, v. 40, no. 2, 1966, 468-470 TOPIC TAGS: ignition temperature, thermite mixture, activation energy ABSTRACT: The previously described method for studying thermal explosions (A. G. Merzhanov, V. G. Abramov, F. I. Dubovitskiy, Dokl. M SSSR, 128, 1238, 1959; V. V. Barzykin, A. G.Merzhanov, Zh. fiz. khim. 38, 2640, 1964.) was modified and used for investigating the reaction kinetics and self-ignition temperature of a thermite mixum consisting of Fe?03 52.5, Al 17.5, and Al 0 30%. The mixture was pressed to form cylindrical specimens with a constant lenghA to diameter ratio 1/d = 0.2, a density p 1 2.3 g/cm3 and a t4ckness varying from 0.095 to 0.320 cm. The specimen was immersed in molten Pb"hnd heated in an electric furnace. The temperature at which a 11surf" ippeared on the lead surface was found to be the critical self-ignition temperature of the thermite specimen. The critical temperature decreased as the thickness of the specimen increased from 810C for a 0.095 cm thick specimen to 676C for a 0.320 cm thick specimen. The activation energ~,and the rate of the Card 1/2 upc: 5411. L 21485,46 ACC NRs A-p6oo8o96 heat of' reaction were calculated to be 4o2ooo cal/mole and 4.5 x 108 cal/g-sec, respectively. Since there is no gas evolution during a thermite reaction, thermite -.mixtures may be used &s simple models for studying thermal explosions and the self- ignition of condensed systems. Orig. art. has: 2 figures, 1 table, and 4 formulas. [PS] SUB CODE: i9/ sm DATE: o5jan65/ ORIG REEF: 007/ ATD PRESS: C --:ACC NR; :AP6011501- SOURCE CODE: UR/0414/65/000/004/0024/0030 -''AUTIIOR*. Hakaiinov, E. I.. (Hoscow); Herzhanov, A. G. (Hoacow); Shkiro,, VV (Ho 3 cow ORG:, none TITLE: Gastess compositions as the simplest combustion model for condensed systems SOURCE: Fizika SorenLya i vzryva, no. 4, 1996, 24-30 TOPIC TAGS: solid propellant, combustion, ombustion instability '-A"TRACT: Condensed phase reactions are of fundamental importance for udyLng solid Provellant combustion.'~ollowever, the presence of gasift- a t cation and gas-phafte re Ction s affects the combustion mech- anism so that the characteristics of the condensed-phase reactions can be studied only with a model-mixture in which no gases are formed. Most of the known thermits have been found to be unsuitable for this purposer since they all exhibited a considerable pressure effect on tile burning ve I oLcity, thus indicating the presence of gas-phase reactions. Therefore, to formulate a thermft which would Lreact only in the con- densed phase, a mixture of 25% Al and 75% Fe203 was diluced with amounts of A1203 90 that the burning temperature was lowered carci 1/ 3 UDC:..:!1536i46+54jr.4Z7.6 -:ACC NR; AP6011501 below the:bolling temperatures of any of its components or products. These mixtures were compacted to densities in the range of 0.1 < olpmax