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kw.\*:("STRUCTURE DEPLOYABLE ESPACE")

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RELIABILITY ESTIMATE OF A SPACE DEPLOYABLE ANTENNA = ESTIMATION DE LA FIABILITE D'UNE ANTENNE SPATIALE DEPLOYABLEMORENO FJ.1973; IN: PROC. 1973 ANNU. RELIAB. MAINTAINABILITY SYMP.; PHILADELPHIA, PA.; 1973; NEW YORK, U.S.A.; INST. ELECTR. ELECTRON. ENG.; DA. 1973; PP. 182-185; BIBL. 2 REF.Conference Paper

ABOUT THE MOTION OF A HEAVY FLEXIBLE STRING ATTACHED TO THE SATELLITE IN THE CENTRAL FIELD OF ATTRACTIONSINGH RB; DEMIN VG.1972; CELEST. MECH.; NETHERL.; DA. 1972; VOL. 6; NO 3; PP. 268-277; ABS. RUSSE; BIBL. 4 REF.Serial Issue

MULTILOOP ATTITUDE CONTROL SYSTEM FOR A SATELLITE WITH FLEXIBLE BOOMS = SYSTEME DE CONTROLE D'ATTITUDE A BOUCLES MULTIPLES POUR UN SATELLITE A MATS FLEXIBLESDI LORENZO R; DE BERNARDIS E.1973; A.G.A.R.D. CONF. PROC.; FR.; DA. 1973; NO 114; PP. 9.1-9.13; BIBL. 18 REF.; (24TH TECH. MEET. AVIONICS PANEL AGARD: AUTOM. MANNED AEROSP. SYST.; DAYTON, OHIO; 1972)Conference Paper

ATTITUDE STABILITY OF A DUAL-SPIN SATELLITE WITH A LARGE FLEXIBLE SOLAR ARRAY = STABILITE D'ATTITUDE D'UN SATELLITE A ROTATION DOUBLE MUNI D'UN GRAND PANNEAU SOLAIRE FLEXIBLECHERCHAS DB; HUGHES PC.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 2; PP. 126-132; BIBL. 28 REF.Serial Issue

DER EINFLUSS DER AERODYNAMISCHEN MOMENTE AUF DIE DREHBEWEGUNG DER PROTON-SATELLITEN = INFLUENCE DES MOMENTS AERODYNAMIQUES SUR LE MOUVEMENT DE ROTATION DES SATELLITES PROTONBELETSKII VV.1973; Z. FLUGWISSENSCH.; DTSCH.; DA. 1973; VOL. 21; NO 2; PP. 55-63; ABS. ANGL. FR.; BIBL. 9 REF.Serial Issue

LOW-COST SOLAR ELECTRIC TEST BED FOR ION THRUSTER SYSTEMSSCHEEL HW.1972; J. SPACECR. ROCK.; U.S.A.; DA. 1972; VOL. 9; NO 12; PP. 853-857; BIBL. 6 REF.Serial Issue

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