Pascal and Francis Bibliographic Databases

Help

Search results

Your search

kw.\*:("SPATIONEF")

Document Type [dt]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Publication Year[py]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Discipline (document) [di]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Language

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Author Country

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Origin

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Results 1 to 25 of 3335

  • Page / 134

Export

Selection :

  • and

ERREURS DE MESURE DES ANGLES DE ROTATION D'UN OBJET PORTEUR DE LA PLATE-FORME GYROSTABILISEE A TROIS AXES, COMPTE TENU DE LA DERIVE DE LA PLATE-FORMEPLOTNIKOV PK.1972; IZVEST. VYSSH. UCHEBN. ZAVED., PRIBOROSTR.; S.S.S.R.; DA. 1972; NO 10; PP. 81-86; BIBL. 4 REF.Serial Issue

THE ROLE OF TESTING IN ACHIEVING AEROSPACE SYSTEMS EFFECTIVENESSSMITH AM; MATTESON TD.1973; IN: PROC. 1973 ANNU. RELIAB. MAINTAINABILITY SYMP.; PHILADELPHIA, PA.; 1973; NEW YORK, U.S.A.; INST. ELECTR. ELECTRON. ENG.; DA. 1973; PP. 36-41Conference Paper

OSCILLATIONS SPATIALES D'UN APPAREIL EN DESCENTE AVEC UN SYSTEME DE STABILISATION NON LINEAIREGROVBOV VA; KUDINENKO AV.1973; KOSM. ISSLEDOV.; S.S.S.R.; DA. 1973; VOL. 11; NO 2; PP. 186-191; BIBL. 3 REF.Serial Issue

PHASE DOUBLE PLANE AS A METHOD TO STUDY THE DYNAMICS OF A SPACECRAFT WITH LIMITED CONSTRUCTIONAL RIGIDITYRUTKOVSKY VY; SUKHANOV VM.1971; IN: PROC. INT. FED. AUTOM. CONTROL 5TH WORLD CONGR.; PARIS; 1972; DUESSELDORF; IFAC; DA. 1971; VOL. 2; PP. 1-7; BIBL. 3 REF.Conference Proceedings

UTILISATION D'UN FILTRE MATHEMATIQUE POUR LA CONSTRUCTION D'UN SYSTEME INERTIEL SANS PLATE-FORME POUR LA STABILISATION D'UN SPATIONEFSIDOROV IM; GONCHAROVA LE; KOZLOVSKAYA AA et al.1972; KOSM. ISSLEDOV.; S.S.S.R.; DA. 1972; VOL. 10; NO 6; PP. 841-849; BIBL. 4 REF.Serial Issue

A QUASI-INERTIAL ATTITUDE MODE FOR ORBITING SPACECRAFT = UN MODE D'ATTITUDE QUASI INERTIEL POUR VEHICULE SPATIAL SUR ORBITEELROD BD.1972; J. SPACECR. ROCK.; U.S.A.; DA. 1972; VOL. 9; NO 12; PP. 889-895; BIBL. 6 REF.Serial Issue

LIAPUNOV STABILITY ANALYSIS OF SPINNING FLEXIBLE SPACECRAFT = ANALYSE DE STABILITE DE LIAPUNOV POUR UN SPATIONEF FLEXIBLE EN MOUVEMENT DE SPINBARBERA FJ; LIKINS P.1973; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 4; PP. 457-466; BIBL. 28 REF.Serial Issue

ALGORITHME POUR LA DETERMINATION DE LA POSITION D'UN OBJET MOBILEFILARETOVA SA.1973; IZVEST. VYSSH. UCHEBN. ZAVED., PRIBOROSTR.; S.S.S.R.; DA. 1973; VOL. 16; NO 1; PP. 68-71; BIBL. 3 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

DERIVEES ISOCHRONES PAR RAPPORT A CERTAINS PARAMETRES DE LA TRAJECTOIRE D'UN SPATIONEFBAKHSHIYAN B TS.1973; KOSM. ISSLEDOV.; S.S.S.R.; DA. 1973; VOL. 11; NO 2; PP. 217-225; BIBL. 5 REF.Serial Issue

LES AUTO-OSCILLATIONS COMPLEXES DES SPATIONEFS PENDANT LA MANOEUVREGAUSHUS EH V; SMOL'YANINOV ND.1973; KOSM. ISSLEDOV.; S.S.S.R.; DA. 1973; VOL. 11; NO 1; PP. 3-13; BIBL. 9 REF.Serial Issue

STRATEGIES FOR CONTROL OF THE SPACE SHUTTLE TRANSITION = STRATEGIES DE COMMANDE DE LA TRANSITION DE LA NAVETTE SPATIALESTENGEL RF.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 1; PP. 77-84; BIBL. 14 REF.Serial Issue

THE THERMAL ANALYSIS OF A BELT TYPE RADIATOR BY THE METHOD OF MATCHED ASYMPTOTIC EXPANSIONSKRANE RJ; JISCHKE MC; RASMUSSEN ML et al.1973; INTERNATION. J. HEAT MASS TRANSFER; G.B.; DA. 1973; VOL. 16; NO 6; PP. 1165-1174; ABS. FR. ALLEM. RUSSE; BIBL. 9 REF.Serial Issue

OPTIMAL PURSUIT IN SPACE = TRAJECTOIRE OPTIMALE DE POURSUITE DANS L'ESPACEHAMZA MH; SALAMA AIA.1973; Z. FLUGWISSENSCH.; DTSCH.; DA. 1973; VOL. 21; NO 5; PP. 173-178; ABS. ALLEM. FR.; BIBL. 6 REF.Serial Issue

TESTING OF SPACECRAFT IN LONG-TERM STORAGE = ESSAI DE SPATIONEF LORS D'UN STOCKAGE DE LONGUE DUREEMASTERSON RJ; MILLER RN.1973; IN: PROC. 1973 ANNU. RELIAB. MAINTAINABILITY SYMP.; PHILADELPHIA, PA.; 1973; NEW YORK, U.S.A.; INST. ELECTR. ELECTRON. ENG.; DA. 1973; PP. 149-155; BIBL. 4 REF.Conference Paper

ABSOLUTE CALIBRATION OF APOLLO LUNAR ORBITAL MASS SPECTROMETERYEAGER PR; SMITH A; JACKSON JJ et al.1973; J. VACUUM SCI. TECHNOL.; U.S.A.; DA. 1973; VOL. 10; NO 2; PP. 348-354; BIBL. 4 REF.Serial Issue

EIN BEITRAG ZUR BERECHNUNG DER AERODYNAMISCHEN KRAFT-UND MOMENTENBEIWERTE VON RAUMFLUGKOERPERN = CONTRIBUTION AU CALCUL DES COEFFICIENTS AERODYNAMIQUES DES FORCES ET DES MOMENTS AUXQUELS SONT SOUMIS LES ENGINS SPATIAUXLUNDERSTADT R; MESCH F.1973; Z. FLUGWISSENSCH.; DTSCH.; DA. 1973; VOL. 21; NO 2; PP. 45-55; ABS. ANGL. FR; BIBL. 16 REF.Serial Issue

DIGITAL AUTOPILOT FOR THE SKYLAB ORBITAL ASSEMBLYTURNBULL JF.1972; NAVIGATION; U.S.A.; DA. 1972; VOL. 19; NO 3; PP. 281-289Serial Issue

ISSLEDOVANIYA PO DINAMIKE POLETA KOSMICHESKIKH APPARATOV = ETUDE DE LA DYNAMIQUE DES VOLS DES SPATIONEFS1973; MOSKVA; NAUKA; DA. 1973; PP. 1-141; BIBL. DISSEM.Book

EXTENDING THE LIFE AND RECYCLE CAPABILITY OF EARTH STORABLE PROPELLANT SYSTEMS = EXTENSION DE LA DUREE DE VIE ET DES POSSIBILITES DE REUTILISATION DES SYSTEMES TERRESTRES A PROPERGOL STOCKABLESCHWEICKERT TF.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 837; PP. 1-8Conference Paper

LE LANCEUR DIAMANT B-P4ROUSSEL JG.1973; AERONAUT. ET ASTRONAUT.; FR.; DA. 1973; NO 39; PP. 5-20; ABS. ANGL. ALLEMSerial Issue

ON-OFF AND ACCELERATION CONTROL OF SOLID ROCKETSMCDONALD AJ.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; NO PART 4; PP. 2576-2585; BIBL. 27 REF.Serial Issue

FORCES ELECTROSTATIQUES PARASITES SUR UNE MASSE D'EPREUVE EN IMPESANTEURBOULAY JL; MAULARD J.1972; OFF. NATION. ET. RECH. AEROSPAT., NOTES TECH.; FR.; DA. 1972; NO 197; PP. 1-56; ABS. ANGL.; BIBL. 2 P. 1/2Serial Issue

24TH TECHNICAL MEETING OF THE AVIONICS PANEL OF AGARD: AUTOMATION IN MANNED AEROSPACE SYSTEMS. DAYTON, OHIO, 16-19 OCTOBER 1972 = EME CONFERENCE TECHNIQUE DE LA COMMISSION AVIONIQUE DE L'AGARD: L'AUTOMATISATION DANS LES SYSTEMES AEROSPATIAUX HABITES. DAYTON, OHIO, 16-19 OCTOBRE 19721973; A.G.A.R.D. CONF. PROC.; FR.; DA. 1973; NO 114; PP. (292 P.); BIBL. DISSEM.; (24TH TECH. MEET. AVIONICS PANEL AGARD: AUTOM. MANNED AEROSP. SYST.; DAYTON, OHIO; 1972)Conference Paper

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

  • Page / 134