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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

PERTURBATION SECULAIRE DES ELEMENTS D'ORBITE DE SATELLITE UTILISANT UNE FORME INTEGRALE APPROCHEE DE LA DENSITE DE L'ATMOSPHERERUDAKOV SA.1976; IN: OBRAB. KOSM. INF.; MOSKVA; NAUKA; DA. 1976; PP. 20-24; BIBL. 4 REF.Book Chapter

ETUDE DU FREINAGE D'UN FAISCEAU ELECTRONIQUE DANS UN RECUPERATEUR DU TYPE SPHERIQUEVOLKOV A YU; DIMITROV SK; MAKHIN AV et al.1982; PRIB. TEH. EKSP.; ISSN 0032-8162; SUN; DA. 1982; NO 1; PP. 48-50; BIBL. 3 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

ACTION DE L'ATMOSPHERE NEUTRE ET IONISEE SUR LE MOUVEMENT D'UN SATELLITE. APPLICATION A LAGEOSMIGNARD F.1981; ANN. GEOPHYS.; ISSN 0003-4029; FRA; DA. 1981; VOL. 37; NO 1; PP. 247-253; ABS. ENG; BIBL. 12 REF.Conference Paper

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

TIME DEPENDENCE OF NEUTRON PULSES IN THE SLOWING DOWN ENERGY REGIONSUMMERFIELD G.1980; TRANSP. THEORY STAT. PHYS.; ISSN 0041-1450; USA; DA. 1980; VOL. 9; NO 1; PP. 27-35; BIBL. 6 REF.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

SYSTEME D'OPTIQUE ELECTRONIQUE, HAUTE TENSION, A SYMETRIE AXIALE, AVEC FORMAGE ELECTROSTATIQUE CENTRIFUGE ET FREINAGE PROFOND DES ELECTRONSANDRIKANIS LI; BUNINA NS.1980; RADIOTEKH. I ELEKTRON.; SUN; DA. 1980; VOL. 25; NO 3; PP. 623-627; BIBL. 5 REF.Article

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

SPIN-REVERSED ACCRETION AS THE CAUSE OF INTERMITTENT SPINDOWN IN SLOW X-RAY PULSARSWANG YM.1981; ASTRON. ASTROPHYS. (BERL.); ISSN 0004-6361; DEU; DA. 1981; VOL. 102; NO 1; PP. 36-44; BIBL. 41 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 DE LA RESISTANCE DE L'ATMOSPHERE SUR L'ORIENTATION GRAVITATIONNELLE UNIAXE D'UN SATELLITE ARTIFICIELSARYCHEV VA; SAZONOV VV.1982; KOSM. ISSLED.; ISSN 0023-4206; SUN; DA. 1982; VOL. 20; NO 5; PP. 659-673; BIBL. 5 REF.Article

UPPER-ATMOSPHERE STUDIES BY RANGING TO SATELLITES.KING HELLE DG.1977; PHILOS. TRANS. R. SOC. LONDON, A; G.B.; DA. 1977; VOL. 284; NO 1326; PP. 555-563; BIBL. 21 REF.Article

THE USAGE OF INTERKOSMOS SATELLITE FOR ASTRODYNAMICS. = UTILISATION DU SATELLITE INTERKOSMOS POUR L'ASTRODYNAMIQUEKLOKOCNIK J; LALA P; NAVARA P et al.1974; NABLJUD. ISKUSSTVEN. SPUTNIK. ZEMLI; S.S.S.R.; DA. 1974 PARU 1975; NO 14; PP. 539-560; ABS. RUSSE; BIBL. 1 P.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

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