SHAPE CHANGE AND CONDUCTION FOR NOSETIPS AT ANGLE OF ATTACK. = CHANGEMENT DE FORME ET CONDUCTION POUR DES POINTES EN INCIDENCECHIN JH.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 5; PP. 599-604; BIBL. 21 REF.Article

TRANSFERTS DE CHALEUR PAR CONVECTION NATURELLE EN MILIEU POREUX1972; EUR-4879 F; LUXEMBOURG; DA. 1972; PP. 1-80; ABS. ANGL.; BIBL. 7 P.Report

VERS LE CALCUL DES CANONS A ELECTRONS AVEC UN JEU THERMIQUE SUIVANT LA METHODE DE SYNTHESEDANILOV VN; SYROVOJ VA.1976; RADIOTEKH. I ELEKTRON.; S.S.S.R.; DA. 1976; VOL. 21; NO 2; PP. 418-421; BIBL. 9 REF.Article

SOME RELIABILITY CHARACTERISTICS OF CRT CATHODE ASSEMBLIES.CORSON BR.1974; I.E.E.E. TRANS. RELIABIL.; U.S.A.; DA. 1974; VOL. 23; NO 4; PP. 226-230; BIBL. 8 REF.Article

PROGETTAZIONE TERMICA, DEGLI SCHERMI, DEI SISTEMI DI COMANDO E STUDI DI SICUREZZA PER SISTEMA DI REFUELING IN REATTORE PER DISSALAMENTO = PROJET THERMIQUE DES ECRANS ET DES SYSTEMES DE COMMANDE, ET ETUDES DE SECURITE POUR LES SYSTEMES DE CHARGEMENT DES REACTEURS POUR LE DESSALEMENTCESARI F; DESSOLIS F; STAMPONE E et al.1972; RT-ING (72)3; ITAL.; DA. 1972; PP. (277 P.); ABS. ANGL.; BIBL. 16 REF.Report

THE STATIONARY FORM OF DESAGREGATING BODIES UNDER RADIATION HEATING IN A HYPERSONIC FLOWBRYKIN MV.1982; TEPLOFIZ. VYS. TEMP.; ISSN 0040-3644; SUN; DA. 1982; NO 2; PP. 283-287; BIBL. 14 REF.Article

TEMPERATURE AND ABLATION OPTICAL SENSORCASSAING JJ; LELIEVRE PM; DURRENBERGER P et al.1981; PROG. ASTRONAUT. AERONAUT.; ISSN 0079-6050; USA; DA. 1981; VOL. 77; PP. 242-259; BIBL. 2 REF.Conference Paper

PROPRIETES ASYMPTOTIQUES DES EQUATIONS DE LA THEORIE DE COUCHE D'ENDOMMAGEMENT DES MATERIAUX DANS LES PROBLEMES DE LA MODIFICATION DE LA FORME DES CORPS LORS DE L'ECHAUFFEMENT AERODYNAMIQUEZNAMENSKIJ VV; LUNEV VV.1981; IZV. AKAD. NAUK SSSR, MEH. ZIDK. GAZA; ISSN 0568-5281; SUN; DA. 1981; NO 1; PP. 46-54; BIBL. 9 REF.Article

CALCULATION OF THE TRANSIENT ABLATION VELOCITYUGLOV AA; SMUROV I YU; ANDRIANOV SS et al.1981; Z. TEH. FIZ.; ISSN 0044-4642; SUN; DA. 1981; VOL. 51; NO 9; PP. 1787-1791; BIBL. 10 REF.Article

HEATSHIELD MATERIALS EROSION AT HYPERSONIC VELOCITIES.MCMILLEN LD; DUNBAR LE; JACKSON D et al.1976; IN: FLUID PLASMA DYN. CONF. 9; SAN DIEGO, CALIF.; 1976; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; VOL. 321; PP. 1-7; BIBL. 2 REF.Conference Paper

FINITE-ELEMENT ANALYSIS FOR CONDUCTION AND ABLATION MOVING BOUNDARYCHIN JH.1981; PROG. ASTRONAUT. AERONAUT.; ISSN 0079-6050; USA; DA. 1981; VOL. 78; PP. 249-265; BIBL. 12 REF.Conference Paper

SOME PROBLEMS CONCERNING THE AUTOMATIZATION OF DESIGNING HEAT PROTECTION SYSTEMS FOR SPACECRAFTSIVANOV AA.1980; INZ.-FIZ. Z.; ISSN 0021-0285; BYS; DA. 1980; VOL. 39; NO 2; PP. 204-210; ABS. ENG; BIBL. 3 REF.Article

RAPID DEPRESSURIZATION OF A THERMAL INSULATION SYSTEM FOR HIGH TEMPERATURE GAS REACTORSARANOVITCH E; VAN ASSELT D.1972; EUR-4880E; LUXEMBOURG; DA. 1972; PP. 1-53Report

LOW TEMPERATURE SIMULATION OF SUBLIMING BOUNDARY-LAYER FLOW IN JUPITER ATMOSPHERE.CHING JEN CHEN.1978; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1978; VOL. 16; NO 3; PP. 259-267; BIBL. 24 REF.Article

CURRENT STATUS AND THE FUTURE OF ADVANCED SUPERSONIC TRANSPORT NOISEO'KEEFE JV; MANGIAROTTY RA; PICKUP N et al.1981; J. AIRCR.; ISSN 0021-8669; USA; DA. 1981; VOL. 18; NO 7; PP. 576-581; BIBL. 11 REF.Article

EFFECTS OF GASEOUS PRODUCTS FROM THE DECOMPOSITION OF HEAT PROTECTION COATING ON HEAT TRANSFER NEAR THE STAGNATION POINT OF A BLUNT BODYBIBERMAN LM; BRONIN S YA; BRYKIN MV et al.1978; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; SUN; DA. 1978; NO 3; PP. 129-136; BIBL. 20 REF.Article

EFFECTS OF SCALED HEATSHIELD TILE MISALIGNMENT ON ORBITER BOUNDARY-LAYER TRANSITION.GOODRICH WD; STALMACH CJ JR.1977; J. SPACECR. ROCK.; U.S.A.; DA. 1977; VOL. 14; NO 10; PP. 638-640; BIBL. 8 REF.Article

QUELQUES PROBLEMES INDUSTRIELS OU LA CONVECTION NATURELLE JOUE UN ROLE IMPORTANTGROSSIN R.1972; REV. GEN. THERM.; FR.; DA. 1972; VOL. 11; NO 126; PP. 543-554Serial Issue

Options for improving rigidized ceramic heatshieldsLEISER, D. B; SMITH, M; STEWART, D. A et al.Ceramic engineering and science proceedings. 1985, Vol 6, Num 7-8, pp 757-768, issn 0196-6219Article

Ceramic composite thermal protection systemsFISHER, R. E; BURKLAND, C. V; BUSTAMANTE, W. E et al.Ceramic engineering and science proceedings. 1985, Vol 6, Num 7-8, pp 806-819, issn 0196-6219Article

Thermal buffer made of He I at constant volumeJAGER, B; MARDION, G. B; CLAUDET, G et al.Cryogenics (Guildford). 1985, Vol 25, Num 10, pp 578-582, issn 0011-2275Article

THE 60-MW SHUTTLE INTERACTION HEATING FACILITYWINOVICH W; CARLSON WCA.1980; J.S.A. TRANS.; USA; DA. 1980; VOL. 19; NO 2; PP. 75-93; BIBL. 20 REF.Article

A PARAMETER CHARACTERIZING THE EFFECT OF THERMOOPTICAL PROPERTIES OF A GLASSY HEAT PROTECTIVE MATERIAL ON ITS MELLING VELOCITY BY RADIATION-CONVECTION HEATINGSENCHENKOV AS.1979; INZHENER.-FIZ. ZH.; BYS; DA. 1979; VOL. 36; NO 4; PP. 588-590; ABS. ENG; BIBL. 6 REF.Article

EFFECT OF CALCIUM SILICATE SUBSTRATE ON THERMAL BARRIER FIRE TESTINGWHITE RH.1982; FORD. PROD. J.; ISSN 0015-7473; USA; DA. 1982; VOL. 32; NO 7; PP. 25-27; BIBL. 9 REF.Article

A DEVICE FOR STUDYING THE DEFORMATION CHARACTERISTICS OF HEAT SHIELDING MATERIALS IN VARYING MEDIA AND PRESSURE WITH UNIFORM AND UNILATERAL HEATINGTRET'YACHENKO GN; GRACHEVA LI.1978; PROBL. PROCHN.; UKR; DA. 1978; NO 7; PP. 114-116Article