THERMAL STRESS ANALYSIS OF REENTRY VEHICLE NOSETIPS AT ANGLE OF ATTACKCROSE JG; MCKINLEY TK.1972; COMPUTERS AND STRUCT.; G.B.; DA. 1972; VOL. 2; NO 5-6; PP. 1031-1042; BIBL. 9 REF.Serial Issue

LE FREINAGE DANS L'ATMOSPHERE D'UN APPAREIL AVEC UN EQUIPAGE APRES UN VOL INTERPLANETAIREKLIMIN AV.1973; KOSM. ISSLEDOV.; S.S.S.R.; DA. 1973; VOL. 11; NO 1; PP. 31-37; BIBL. 9 REF.Serial Issue

LENKMETHODEN FUER WAERMEOPTIMALE DREIDIMENSIONALE ABSTIEGSBAHNEN VON AERODYNAMISCHEN WIEDEREINTRITTSKOERPERN = METHODES DE GUIDAGE SUR UNE TRAJECTOIRE TRIDIMENSIONNELLE OPTIMISEE CONTRE L'ECHAUFFEMENT DES CORPS DE RENTREE AERODYNAMIQUESKONIG H.1973; Z. FLUGWISSENSCH.; DTSCH.; DA. 1973; VOL. 21; NO 1; PP. 32-43; ABS. ANGL. FR.; BIBL. 4 REF.Serial Issue

OPTIMAL LIFT CONTROL BY MIELE'S METHOD FOR THE ATMOSPHERIC ENTRY OF A HYPERSONIC GLIDER. II. ISOPERIMETRIC TYPE PROBLEMSBEINER L.1972; REV. ROUMAINE SCI. TECH., MEC. APPL.; ROUMAN.; DA. 1972; VOL. 17; NO 5; PP. 1039-1053; BIBL. 2 REF.Serial Issue

COLLISION LESS PLASMA FLOW OVER A CONDUCTING SPHERESTONE NH; ORAN WA; URI SAMIR et al.1972; PLANET. SPACE SCI.; G.B.; DA. 1972; VOL. 20; NO 10; PP. 1787-1790; BIBL. 8 REF.Serial Issue

USE OF MAGNETOMETERS AND ASYMMETRIC ANTENNA PATTERNS FOR ATTITUDE DETERMINATION = UTILISATION DE MAGNETOMETRES ET DE DIAGRAMMES ASYMETRIQUES D'ANTENNES POUR LA DETERMINATION D'ATTITUDEDELFICO AN; GRAEDEL TE; PRINGLE R JR et al.1972; J. SPACECR. ROCK.; U.S.A.; DA. 1972; VOL. 9; NO 12; PP. 903-908; BIBL. 2 REF.Serial Issue

FLIGHT TEST CORRELATION TECHNIQUE FOR TURBULENT BASE HEAT TRANSFER WITH LOW ABLATION = TECHNIQUE DE CORRELATION D'ESSAIS EN VOL POUR LE TRANSFERT DE CHALEUR TURBULENT AU CULOT AVEC FAIBLE ABLATIONBULMER BM.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 3; PP. 222-224; BIBL. 6 REF.Serial Issue

FRACTURE TOUGHNESS OF CARBON-CARBON COMPOSITES = TENACITE DE RUPTURE DES COMPOSITES CARBONE-CARBONEGUESS TR; HOOVER WR.1973; J. COMPOSITE MATER.; U.S.A.; DA. 1973; VOL. 7; NO 1; PP. 2-20; BIBL. 19 REF.Serial Issue

SPACE STRUCTURESFOREST JD; CHRISTIAN JL.1973; A.S.T.M. SPEC. TECH. PUBL.; U.S.A.; DA. 1973; NO 524; PP. 134-162; BIBL. 17 REF.Serial Issue

MASS SPECTROMETRIC CAPTURE AND ANALYSIS OF THE ABLATION PRODUCTS FROM HYPERSONIC PROJECTILESBIHL S; JOECKLE B; SONTAG A et al.1972; ISL-25-72; FR.; DA. 1972; PP. (13 P.); BIBL. 1 REF.Report

HYPERSONIC TRANSITIONAL AND TURBULENT FLOW STUDIES A LIFTING ENTRY VEHICLE = ETUDES D'ECOULEMENT HYPERSONIQUE DE TRANSITION ET TURBULENT SUR UN VEHICULE DE RENTREE PLANANTEYOUNG CH; REDA DC; ROBERGE AM et al.1972; J. SPACECR. ROCK.; U.S.A.; DA. 1972; VOL. 9; NO 12; PP. 883-888; BIBL. 18 REF.Serial Issue

ESTIMATION ANALYTIQUE DE L'INFLUENCE DE LA MOBILITE D'UNE PETITE MASSE INTERNE SOUS LES OSCILLATIONS D'UN CORPS LORS DU FREINAGE DANS L'ATMOSPHERESHILOV AA.1972; DOKL. AKAD. NAUK S.S.S.R.; S.S.S.R.; DA. 1972; VOL. 207; NO 5; PP. 1074-1077; BIBL. 2 REF.Serial Issue

ASYMMETRIC NOSE BLUNTNESS EFFECTS ON THE AERODYNAMICS OF A SLENDER CONE AT MACH 14 = EFFETS D'EMOUSSEMENT ASYMETRIQUE DE LA POINTE SUR L'AERODYNAMIQUE D'UN CONE ELANCE A MACH 14WALCHNER O.sdIN: AIAA 2ND ATMOS. FLIGHT MECH. CONF. PALO ALTO, CALIF., 1972; S.L.; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; PP. 1-6; BIBL. 5 REF.Conference Paper

TOTAL ENTHALPY-MEASUREMENT FROM BLUNT BODY GAS CAP EMISSION IN ARC-HEATED WIND TUNNELS: RESULTS AND APPLICATIONLAWRENCE LR JR; DOYLE JP JR; WEEKS TM et al.sdIN: AIAA 7TH AERODYN. TES. CONF. PALO ALTO, CALIF., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; NO 993; PP. 1-11; BIBL. 17 REF.Conference Paper

DETECTION OF FLIGHT VEHICLE TRANSITION FROM BASE MEASUREMENTS = DETECTION DE LA TRANSITION SUR DES VEHICULES EN VOL A PARTIR DE MESURES AU CULOTBULMER BM.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 4; PP. 280-281; BIBL. 2 REF.Serial Issue

ALGORITHME ADAPTATIF DE LA STABILISATION D'UN SPATIONEF LORS DE LA RENTREE DANS L'ATMOSPHEREOKHOTSIMSKIJ DE; SIKHARULIDZE YU G.1973; IZVEST. AKAD. NAUK S.S.S.R., TEKH. KIBERN.; S.S.S.R.; DA. 1973; NO 2; PP. 160-167; BIBL. 5 REF.Serial Issue

DEVELOPMENT OF AN UNSTEADY WATER TUNNELSCHUTZENHOFER L; MORROW D; SHIH C et al.sdIN: AIAA 7TH AERODYN. TEST. CONF. PALO ALTO, CALIF., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; NO 993; PP. 1-10; BIBL. 10 REF.Conference Paper

HEAT-TRANSFER AND ABLATION-RATE CORRELATIONS FOR RE-ENTRY HEAT-SHIELD AND NOSETIP APPLICATIONS = CORRELATIONS DE TRANSFERT DE CHALEUR ET DE VITESSE D'ABLATION POUR APPLICATIONS AUX POINTES ET BOUCLIERS THERMIQUES DE RENTREEPUTZ KE; BARTLETT EP.1973; J. SPACEER. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 1; PP. 15-22; BIBL. 20 REF.Serial Issue

THE NUMERICAL SOLUTION OF CONVECTIVE HEAT TRANSFER IN THE SPACE SHUTTLE BASE REGION BY TELENIN'S METHODHENG JCS.1973; LECTURE NOTES PHYS.; GERM.; DA. 1973; NO 19; PP. 191-200; BIBL. 7 REF.; (PROC. 3RD INT. CONF. NUMER. METHODS FLUID MECH II. PROBL. FLUID MECH.; PARIS; 1972)Conference Paper

A MECHANISM FOR ABLATION-INDUCED SPIN-UP = MECANISME DE L'ACCELERATION ANGULAIRE INDUITE PAR ABLATIONERICSON LE; PRICE DA JR.1973; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 4; PP. 567-569; BIBL. 20 REF.Serial Issue

COMPARISON OF THREE OSCILLATORY TECHNIQUES FOR CONES AT INCIDENCE = COMPARAISON DE TROIS TECHNIQUES OSCILLATOIRES POUR DES CONES EN INCIDENCEORLIK RUCKEMANN KJ; IYENGAR S; LABERGE JG et al.sdIN: AIAA 7TH AERODYN. TEST. CONF. PALO ALTO, CALIF., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; NO 993; PP. 1-7; BIBL. 9 REF.Conference Paper