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DIE WIRTSCHAFTLICHE VERWENDUNG VON BLECHEN IM FLUGZEUGBAU = L'UTILISATION ECONOMIQUE DES TOLES DANS LA FABRICATION DES AVIONS1973; INDUSTR.-ANZ.; DTSCH.; DA. 1973; VOL. 95; NO 10; PP. 168-170Serial Issue

IMPIEGO DELL'ALLUMINIO NEGLI AEREI MODERNI = EMPLOI DE L'ALUMINIUM DANS LES AVIONS MODERNES1972; ALLUMINIO; ITAL.; DA. 1972; VOL. 41; NO 11-12; PP. 595-598Serial Issue

COMPUTER INTERACTIVE GRAPHICS IN AEROSPACE ENGINEERING DESIGN EDUCATION.SMITH HW.1976; IN: AIRCR. SYST. TECHNOL. MEET. AM. INST. AERONAUT. ASTRONAUT.; DALLAS, TEX.; 1976; NEW YORK; AIAA; DA. 1976; PP. 1-11; BIBL. 12 REF.Conference Paper

STRESSKIN ADDS TO PAYLOAD = LES STRUCTURES STRESSKIN PERMETTENT D'AUGMENTER LE POIDS UTILE1973; IRON AGE METALWORKG INTERNATION.; U.S.A.; DA. 1973; VOL. 12; NO 2; PP. 26; ABS. ALLEM. FR. ESPSerial Issue

COST ANALYSIS AS APPLIED TO AIRCRAFT SYNTHESIS = ANALYSE DU COUT APPLIQUEE A LA SYNTHESE DES AVIONSFISHER JF; HITCHCOCK ST; TRELEASE RH et al.sdIN: SOC. AERONAUT. WEIGHT ENG. INC. 31ST ANNU. CONF. ATLANTA, 1972; LOS ANGELES; S.A.W.E.; DA. S.D.; VOL. 913; PP. 1-25; BIBL. 5 REF.Conference Paper

AN APPROACH TO SYSTEM COST OPTIMIZATION = APPROCHE D'UN SYSTEME D'OPTIMISATION DU COUTGUINN SL.sdIN: SOC. AERONAUT. WEIGHT ENG. INC. 31ST ANNU. CONF. ATLANTA, 1972; LOS ANGELES; S.A.W.E.; DA. S.D.; VOL. 941; PP. (48 P.)Conference Paper

A MIXED OPTIMIZATION METHOD FOR AUTOMATED DESIGN OF FUSELAGE STRUCTURES = UNE METHODE MIXTE D'OPTIMISATION POUR LA CONCEPTION AUTOMATIQUE DE STRUCTURES DE FUSELAGESOBIESZCZANSKI J; LOENDORF D.1972; J. AIRCR.; U.S.A.; DA. 1972; VOL. 9; NO 12; PP. 805-811; BIBL. 16 REF.Serial Issue

LE NORSIAL, MATERIAU D'AVENIR DANS LES TECHNIQUES AEROSPATIALESSPINCOURT J.1973; INTERAVIA; SUISSE; DA. 1973; VOL. 28; NO 4; PP. 352Serial Issue

L'AVIATION GENERALE EN FRANCE1973; INTERAVIA; SUISSE; DA. 1973; VOL. 28; NO 5; PP. 498-500Serial Issue

INTERACTIVE 3D SHAPE DESIGN. MULTIPATCH AND MULTIOBJECT = CREATION CONVERSATIONNELLE DE FORMES EN 3 DIMENSIONS. MULTI-MORCEAU ET MULTI-OBJETARMIT AP.1973; AIRCR. ENGNG; G.B.; DA. 1973; VOL. 45; NO 2; PP. 13-17; BIBL. 4 REF.Serial Issue

THE DESIGN AND APPLICATION OF THE TRAVERSING INFRA-RED INSPECTION SYSTEM-TIRISCOHEN SE.1973; NON-DESTRUCT. TESTG; G.B.; DA. 1973; VOL. 6; NO 2; PP. 74-80; BIBL. 11 REF.Serial Issue

GOVERNMENT ASSISTANCE FOR TECHNICAL INFORMATION IN INDUSTRY AND SIMPLE MECHANIZATION FOR SMALL INFORMATION CENTRES. 25 TH. MEETING OF THE AGARD TECHNICAL INFORMATION PANEL. ANKARA, TURKEY, 23-24 OCTOBER 19721973; A.G.A.R.D. CONF. PROC.; FR.; DA. 1973; NO 117; PP. (99 P.); BIBL. DISSEM.Conference Paper

THE EARLY DETECTION OF FATIGUE DAMAGE BY EXOELECTRON EMISSION AND ACOUSTIC EMISSIONMOORE JF; TSANG S.1972; A.S.T.M. SPEC. TECH. PUBL.; U.S.A.; DA. 1972; NO 515; PP. 143-157; BIBL. 1 P.; (TEST. PREDICT. MATER. PERFORMANCE STRUCT. COMPONENTS. SYMP.; I. II. ANAHEIM, CALIF.-ATLANTIC CITY, N.J.; 1971)Conference Paper

PREPRINTS OF THE SCIENTIFIC PROGRAM/AEROSPACE MEDICAL ASSOCIATION 1982 ANNUAL SCIENTIFIC MEETING, BAL HARBOUR FL, MAY 10-13, 19821982; AEROSPACE MEDICAL ASSOCIATION. ANNUAL SCIENTIFIC MEETING/1982-05-10/BAL HARBOUR FL; USA; WASHINGTON: AMERICAN MEDICAL ASSOCIATION; DA. 1982; 329 P.; 28 CMConference Proceedings

CUSPED MAGNETIC FIELD MERCURY ION THRUSTER.BEATTIE JR; WILBUR PJ.1977; J. SPACECR. ROCK.; U.S.A.; DA. 1977; VOL. 14; NO 12; PP. 747-755; BIBL. 19 REF.Article

L'AERODYNAMIQUE DU LANCEUR ARIANNE.BOUCHET J; BEC R.1977; CENTRE NATION. ET. SPATIALES, NOTE TECH.; FR.; DA. 1977; NO 75; PP. 1-27; H.T. 22; ABS. ANGL.Serial Issue

INTERNATIONAL SYMPOSIUM ON SPACE TECHNOLOGY AND SCIENCE. 11. PROCEEDINGS; TOKYO; 1975.1975; TOKYO; AGNE; DA. 1975; PP. (1049P.); BIBL. DISSEM.Conference Proceedings

L'INDUSTRIE AEROSPATIALE AMERICAINE: SITUATION ACTUELLE ET PERSPECTIVES D'AVENIRGEDDES JP.1973; INTERAVIA; SUISSE; DA. 1973; VOL. 28; NO 5; PP. 518-524Serial Issue

L'AVIATION EN AUSTRALASIE. I. LA PRODUCTION AERONAUTIQUEMUIR N.1973; INTERAVIA; SUISSE; DA. 1973; VOL. 28; NO 3; PP. 254-256Serial Issue

La fusée VASIMR = The VASIMR rocketCHANG DIAZ, Franklin.Pour la science. 2001, Num 279, pp 50-59, issn 0153-4092Article

ISRAEL ANNUAL CONFERENCE ON AVIATION AND ASTRONAUTICS. 18. PROCEEDINGS; TEL AVIV-HAIFA; 1976.1976; ISRAEL J. TECHNOL.; ISRAEL; DA. 1976; VOL. 14; NO 1-2; PP. 1-114; BIBL. DISSEM.Conference Paper

SINUSOIDAL IMPUT DESCRIBING FUNCTION FOR HYSTERESIS FOLLOWED BY ELEMENTARY BACKLASH.RINGLAND RF.1976; I.E.E.E. TRANS. AUTOMAT. CONTROL; U.S.A.; DA. 1976; VOL. 21; NO 2; PP. 285-288; BIBL. 1 REF.Article

LOCHSTREIFENGERAET REPRODUZIERT FLUGMESSDATEN. II. = UN DISPOSITIF A BANDES PERFOREES REPRODUIT LES PARAMETRES DE VOLJANSEN D.1974; ELEKTRONIK; DTSCH.; DA. 1974; VOL. 23; NO 5; PP. 171-175Article

PRECISION POINTING AND TRACKING I.1973; IN: 14TH JT. AUTOM. CONTROL CONF. AM. AUTOM. CONTROL COUNC.; COLUMBUS, OHIO; 1973; NEW YORK; INST. ELECTR. ELECTRON. ENG.; DA. 1973; PP. 788-797; BIBL. DISSEM.Conference Paper

PROCEEDINGS OF THE 15TH ISRAEL ANNUAL CONFERENCE ON AVIATION AND ASTRONAUTICS. TEL AVIV, 14-15 MARCH 1973 = TRAVAUX DE LA 15EME CONFERENCE ANNUELLE D'ISRAEL SUR L'AVIATION ET L'ASTRONAUTIQUE. TEL AVIV-HAIFA-14 ET 15 MARS 19731973; ISRAEL J. TECHNOL.; ISRAEL; DA. 1973; VOL. 11; NO 1-2; PP. 1-111; BIBL. DISSEM.Conference Paper

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