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L'INFLUENCE DU FREINAGE ATMOSPHERIQUE SUR LE MOUVEMENT D'UN SATELLITE SUIVANT UNE ORBITE A GRANDE EXCENTRICITEFOMINOV AM.1974; BJULL. INST. TEOR. ASTR.; S.S.S.R.; DA. 1974; VOL. 13; NO 9; PP. 571-578; ABS. ANGL.; BIBL. 4 REF.Article

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

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

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

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

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

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

THE APPLICATION OF MODEL ATMOSPHERES TO SYNCHRONOUS SATELLITE LAUNCHES.HOLBROOK JAD.1975; C.A.S.I. TRANS., OTTAWA; CANADA; DA. 1975; VOL. 8; NO 1; PP. 25-28; BIBL. 3 REF.Article

INTERPRETATION OF SHORT PERIOD DENSITY CHANGES SHOWN BY THE DRAG OF SATELLITES.BENCZE P.1974; SPACE RES.; NETHERL.; DA. 1974; VOL. 14; PP. 137-141; BIBL. 8 REF.; (OPEN MEET. WORK. GROUPS 16TH PLENARY MEET. COSPAR. PROC.; CONSTANCE; 1973)Conference Paper

CONTRIBUTION A L'ETUDE DE L'ATMOSPHERE TERRESTRE SUPERIEURE A PARTIR DE L'ANALYSE ORBITALE DES SATELLITES.VERCHEVAL J.1974; ACAD. R. BELG., MEM. CL. SCI., COLLECT. IN-8O; BELG.; DA. 1974; VOL. 41; NO 6; PP. 1-183; ABS. ANGL.; BIBL. 12 P. 1/2Article

INFLUENCE OF SATELLITE AERODYNAMICS ON ATMOSPHERIC DENSITY DETERMINATIONKARR GR; SMITH RE.sdIN: INT. CONF. AEROSP. AERONAUT. METEOROL. WASHINGTON, D.C., 1972; BOSTON, MASS.; AM. METEOROL. SOC.; DA. S.D.; PP. 103-108; BIBL. 7REF.Conference Proceedings

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

ANALYSIS OF THE ORBIT OF 1970-144 F IN ITS LAST 20 DAYS.KING HELE DG.1976; PLANET. SPACE SCI.; G.B.; DA. 1976; VOL. 24; NO 1; PP. 1-16; BIBL. 20 REF.Article

MEASUREMENTS OF UPPER-ATMOSPHERE ROTATIONAL SPEED FROM CHANGES IN SATELLITE ORBITSKING HELE DG.1972; SPACE RES.; NETHERL.; DA. 1972; VOL. 12; PART. 2; PP. 847-855; BIBL. 15REF.Serial Issue

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

EVALUATION GARANTIE DE LA PRECISION DE CONSTRUCTION D'UN MODELE NON SPHERIQUE DE LA DENSITE DE LA HAUTE ATMOSPHERE D'APRES LES OBSERVATIONS DU FREINAGE D'UN SATELLITEVINGARDT DT.1976; KOSM. ISSLED.; S.S.S.R.; DA. 1976; VOL. 14; NO 1; PP. 29-35; BIBL. 5 REF.Article

SYSTEMATIC WINDS AT HEIGHTS BETWEEN 350 AND 675 KM FROM ANALYSIS OF THE ORBITS OF FOUR BALLOON SATELLITES.SLOWEY JW.1975; PLANET. SPACE SCI.; G.B.; DA. 1975; VOL. 23; NO 5; PP. 879-886; BIBL. 16 REF.Article

A SEARCH FOR LUNAR TIDES IN THE THERMOSPHERE.JACCHIA LG.1975; J. GEOPHYS. RES.; U.S.A.; DA. 1975; VOL. 80; NO 10; PP. 1374-1375; BIBL. 3 REF.Article

ATMOSPHERIC DENSITY AND THE ACCURACY OF DETERMINATION OF THE DRAG COEFFICIENT OF A SATELLITEMAROV MY; PYARNPUU AA; ZMIEVSKAYA GI et al.1972; SPACE RES.; NETHERL.; DA. 1972; VOL. 12; PART. 1; PP. 721-726; BIBL. 7 REF.Serial Issue

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