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PERTURBATIONS DE GRANDE PERIODE DES ELEMENTS DE L'ORBITE INTERMEDIAIRE D'UN SATELLITE TERRESTRENOSKOV BN.1974; NABLJUD. ISKUSSTVEN. SPUTNIK. ZEMLI; S.S.S.R.; DA. 1974 PARU 1975; NO 14; PP. 41-52; BIBL. 4 REF.Article

A REVIEW OF SATELLITE LIFETIME AND ORBIT DECAY PREDICTIONDE LAFONTAINE J; GARG SC.1980; U.T.I.A.S. REV.; CAN; DA. 1980; NO 43; 81 P.; BIBL. 94 REF.Serial Issue

COMMENT ON THE PAPER "SOME INVESTIGATIONS INTO THE ATMOSPHERIC DRAG PROBLEM" BY A. H. JUPPKING HELE DG.1978; CELEST. MECH.; NLD; DA. 1978; VOL. 18; NO 2; PP. 163-164; BIBL. 6 REF.Article

REPRESENTATION INTEGRALE DE LA DENSITE DE LA HAUTE ATMOSPHERE LORS DES CALCULS D'ORBITES DE SATELLITESUVOROV GS.1976; IN: OBRAB. KOSM. INF.; MOSKVA; NAUKA; DA. 1976; PP. 13-19; BIBL. 2 REF.Book Chapter

EFFET DU FREINAGE ATMOSPHERIQUE ET DE LA TRAINEE ELECTRIQUE SUR LA TRAJECTOIRE DU SATELLITE LAGEOSAFONSO G; BARLIER F; BERGER C et al.1980; C. R. HEBD. SEANCES ACAD. SCI, SER. B; ISSN 0302-8437; FRA; DA. 1980; VOL. 290; NO 19; PP. 445-448; ABS. ENG; BIBL. 15 REF.Article

ORBITAL DECAY IN A DYNAMIC ATMOSPHEREDE LAFONTAINE J.1979; UTIAS TECH. NOTE; ISSN 0082-5263; CAN; DA. 1979; NO 244; 18 P.; BIBL. 87 P.Serial Issue

ANALYSIS OF THE INCLINATION VARIATIONS OF INTERKOSMOS 10SEHNAL L; KLOKOCNIK J.1979; BULL. AST. INST. CZECHOSL.; CSK; DA. 1979; VOL. 30; NO 4; PP. 205-214; ABS. RUS; BIBL. 15 REF.Article

SYSTEME DE CONTROLE D'ORBITE ET D'ATTITUDE.DUCHON P.sdIN: TECHNOL. SPAT. COURS. OBS. TERRE; TOULOUSE; 1976; TOULOUSE; CENT. NATL. ETUD. SPAT.; DA. S.D.; PP. (57P.); BIBL. 3 REF.Conference Paper

DIURNAL DENSITY VARIATIONS MEASURED BY THE SAN MARCO 3 SATELLITE IN THE EQUATORIAL ATMOSPHERE.BROGLIO L; ARDUINI C; BUONGIORNO C et al.1976; J. GEOPHYS. RES.; U.S.A.; DA. 1976; VOL. 81; NO 7; PP. 1335-1349; BIBL. 20 REF.Article

EFFECTS OF SOLAR RADIATION PRESSURE AND AERODYNAMICFORCES ON SATELLITE-ATTITUDE DYNAMICS AND THEIR UTILIZATION FOR CONTROL: A SURVEY.SHRIVASTAVA SK.1976; J. INDIAN INST. SCI.; INDIA; DA. 1976; VOL. 58; NO 9; PP. 391-411; BIBL. 7 P.Article

ROLE MAJEUR DE LA TRAINEE ELECTRIQUE DANS LA DECROISSANCE SECULAIRE DU DEMI-GRAND AXE DU SATELLITE LAGEOSAFONSO GERMANO BRUNO.1980; ; FRA; DA. 1980; 66 P.; 30 CM; BIBL. 40 REF.; TH. 3E CYCLE: PHYS., PHYS. SPAT./PARIS 6/1980Thesis

DENSITY MODELS FOR THE UPPER ATMOSPHEREDOWD DL; TAPLEY BD.1979; CELEST. MECH.; NLD; DA. 1979; VOL. 20; NO 3; PP. 271-295; BIBL. 12 REF.Article

EFFECTS OF ATMOSPHERIC WINDS AND AERODYNAMIC LIFT ON THE INCLINATION OF THE ORBIT OF THE S3-1 SATELLITE.CHING BK; HICKMAN DR; STRAUS JM et al.1977; J. GEOPHYS. RES.; U.S.A.; DA. 1977; VOL. 82; NO 10; PP. 1474-1480; BIBL. 20 REF.Article

EXOSPHERIC DENSITY MEASUREMENTS FROM THE DRAG-FREE SATELLITE TRIAD.MOE K; DEBRA DB; VAN PATTEN RA et al.1976; J. GEOPHYS. RES.; U.S.A.; DA. 1976; VOL. 81; NO 22; PP. 3753-3761; BIBL. 26 REF.Article

INFLUENCE DES FLUCTUATIONS DE LA DENSITE DE L'ATMOSPHERE SUR LA PRECISION DE DETERMINATION ET DE PREVISION DES ORBITES DE SATELLITES ARTIFICIELS DE LA TERREEHL'YASBERG PE.1981; KOSM. ISSLED.; ISSN 0023-4206; SUN; DA. 1981; VOL. 19; NO 6; PP. 803-812; BIBL. 7 REF.Article

EDDY CURRENT TORQUES, AIR TORQUES, AND THE SPIN DECAY OF CYLINDRICAL ROCKET BODIES IN ORBITWILLIAMS V; MEADOWS AJ.1978; PLANET. SPACE SCI.; GBR; DA. 1978; VOL. 26; NO 8; PP. 721-726; BIBL. 11 REF.Article

TOTAL INTENSITY OF THE DENSITY CHANGES IN THE UPPER-ATMOSPHERE DURING A GEOMAGNETIC STORM.ALMAR I.1974; NABLJUD. ISKUSSTVEN. SPUTNIK. ZEMLI; S.S.S.R.; DA. 1974 PARU 1975; NO 14; PP. 389-402; ABS. RUSSE; BIBL. 9 REF.Article

LE PROBLEME DE L'UTILISATION DES MICROACCELERATEURS DE SATELLITES DANS LE BUT D'ETUDIER LA HAUTE ATMOSPHEREVERESH F.1974; NABLJUD. ISKUSSTVEN. SPUTNIK. ZEMLI; S.S.S.R.; DA. 1974 PARU 1975; NO 14; PP. 499-598; BIBL. 2 REF.Article

ATMOSPHERIC DENSITY VALUES AT 280 KM DEDUCED FROM SPIN DRAG DATA OF THE ROCKET 1965-11DMIOC V.1982; REVUE ROUMAINE DE PHYSIQUE; ISSN 0035-4090; ROM; DA. 1982; VOL. 27; NO 8; PP. 761-765; BIBL. 12 REF.Article

COMPARISON OF ATMOSPHERIC DENSITY DATA FROM MASS SPECTROMETERS AND ATMOSPHERIC DRAG ON THE AEROS SATELLITESROEMER M; FRAMKE W; KRANKOWSKY D et al.1979; J. GEOMAGN. GEOELECTR.; JPN; DA. 1979; VOL. 31; SUPPL.; PP. S71-S79; BIBL. 9 REF.Conference Paper

THEORY OF THE ARTIFICIAL SATELLITE MOTION.ABALAKINE V.1976; IN: GEODYN. SPAT. COURS; LANNION; 1974; TOULOUSE; CENT. NATL. ETUD. SPAT.; DA. 1976; PP. 33-37; BIBL. 3 P.Conference Paper

METHODE D'ETUDE DES CORRECTIONS EST-OUEST POUR UN SATELLITE SYNCHROME SOUMIS AUX PERTURBATIONS DU POTENTIEL TERRESTRE.ESTERLE A.1976; CENTRE NATION. ET. SPATIALES, NOTE TECH.; FR.; DA. 1976; NO 40; PP. 1-18; H.T. 6; ABS. ANGL.; BIBL. 2 REF.Serial Issue

ETUDE DES VENTS DANS LA HAUTE ATMOSPHERE A L'AIDE DE SATELLITEPAAL A.1976; IDOJARAS; MAGYAR.; DA. 1976; VOL. 80; NO 6; PP. 350-355; ABS. ANGL. RUSSE; BIBL. 6 REF.Article

VARIATION DE LA ROTATION DE 16 SATELLITES TERRESTRESNAGY SH.1974; NABLJUD. ISKUSSTVEN. SPUTNIK. ZEMLI; S.S.S.R.; DA. 1974 PARU 1975; NO 14; PP. 483-497; ABS. ANGL.; BIBL. 7 REF.Article

TWIN PROBES FOR SPACE GEODESYBERTOTTI B.1978; NUOVO CIMENTO, C; ITA; DA. 1978; VOL. 1; NO 4; PP. 299-314; ABS. ITA/RUS; BIBL. 33 REF.Article

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