THERMOPILES FOR SPACE APPLICATIONS.FABBRICOTTI M.1973; IN: 4EME JOURN. OPT. SPAT., MARSEILLE; 1973; PARIS; CENT. NATL. ETUD. SPAT.; DA. 1973; PP. 323-334; ABS. FR.; BIBL. 7 REF.Conference Paper

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WHY AND HOW OF HIGH RELIABILITY ELECTRONIC COMPONENTS FOR SPACE APPLICATION.SINHA AK.1977; J. INSTIT. ELECTRON. TELECOMMUNIC. ENGRS; INDIA; DA. 1977; VOL. 23; NO 1; PP. 24-28; BIBL. 5 REF.Article

DES VIDICONS A HAUTE RESOLUTION POUR APPLICATIONS SPATIALES ET MILITAIRES.PARIS G.1977; ELECTRON. APPL. INDUSTR.; FR.; DA. 1977; NO 231; PP. 14-15Article

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DEMAND-TYPE GAS SUPPLY SYSTEM FOR ROCKET BORNE THIN-WINDOW PROPORTIONAL COUNTERS.ACTON LW; CARAVALHO R; CATURA RC et al.1977; REV. SCI. INSTRUM.; U.S.A.; DA. 1977; VOL. 48; NO 11; PP. 1504-1506; BIBL. 3 REF.Article

VIKING '75: THE DEVELOPMENT OF A RELIABLE FLIGHT PROGRAMCLAUSSEN BA II.1977; COMPSAC 77. INTERNATIONAL COMPUTER SOFTWARE AND APPLICATIONS CONFERENCE. 1/1977-11-08/CHICAGO; USA; NEW YORK: IEEE; DA. 1977; 33-37Conference Paper

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ELECTRIC POWER SYSTEMS FOR SPACE. A PROGRESS REPORT.TURNER GF.1975; ASTRONAUT. AND AERONAUT.; U.S.A.; DA. 1975; VOL. 13; NO 12; PP. 18-29Article

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