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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

A SOLID STATE LINEAR INDICATOR FOR AVIONIC DISPLAY SYSTEMSGRATZE SC; LOKER T.1973; MARCONI REV.; G.B.; DA. 1973; VOL. 36; NO 188; PP. 57-66Serial Issue

PRODUCTION DE FAISCEAUX D'ELECTRONS POUR DES TRAVAUX TECHNOLOGIQUES ET DE RECHERCHE DANS LE COSMOS)PATON BE; WAZARENKO OK; PATS'ORA SK et al.1975; KOSM. ISSLEDOV. UKRAINE; S.S.S.R.; DA. 1975; NO 6; PP. 3-7; BIBL. 4 REF.Article

A NEW FAMILY OF MICROELECTRONIC PACKAGES FOR AVIONICS.SETTLE RE JR.1978; SOLID. STATE TECHNOL.; USA; DA. 1978; VOL. 21; NO 6; PP. 54-58; BIBL. 6 REF.Article

CREW RADIATION DOSIMETRY FOR THE MANNED SPACE PROGRAM.TRAVIS CM; COPELAND AC.1976; IN: ADV. INSTRUM. ANNU. I.S.A. CONF. EXHIB. 31. PROC.; HOUSTON, TEX.; 1976; PITTSBURGH, PA.; INSTRUM. SOC. AM.; DA. 1976; VOL. 2; PP. 658.1-658.6Conference Paper

PROTECTION TECHNIQUE FOR CHANNELTRONS IN SPACE RESEARCH.CERULLI IRELLI P; EGIDI A; MARANGONI G et al.1975; REV. SCI. INSTRUM.; U.S.A.; DA. 1975; VOL. 46; NO 4; PP. 417-419; BIBL. 8 REF.Article

THREE TYPES OF SOLID STATE REMOTE POWER CONTROLLERS.BAKER DE.1975; IN: PESC'75. POWER ELECTRON. SPEC. CONF.; CULVER CITY, CALIF.; 1975; NEW YORK; INST. ELECTR. ELECTRON. ENG.; DA. 1975; PP. 151-160Conference Paper

ANALYSE DU FONCTIONNEMENT DES SUSPENSIONS CRYOGENIQUES POUR VEHICULES SPATIAUXRYABOV BA; GORSHKOV VA; RYABOV AB et al.1972; KOSM. ISSLEDOV.; S.S.S.R.; DA. 1972; VOL. 10; NO 4; PP. 515-519; BIBL. 2 REF.Serial Issue

HIGH RESOLUTION LED DISPLAYS FOR ANIONIC APPLICATIONSWICKENDEN DK.1980; DISPLAYS; GBR; DA. 1980; VOL. 2; NO 2; PP. 71-75; BIBL. 5 REF.Article

DIGITAL COMPUTATION MAKES AFCS MORE RELIABLERAYMOND RG; LARSON JC.1975; I.E.E.E. TRANS. AEROSPACE ELECTRON. SYST.; U.S.A.; DA. 1975; VOL. 11; NO 5; PP. 851-861; BIBL. 3 REF.Article

HIGH RELIABILITY PHOTODIODES FOR SPACE APPLICATIONS.BRILMAN M.1975; MICROELECTRON. AND REABIL.; G.B.; DA. 1975; VOL. 14; NO 3; PP. 305-307; H.T. 1Article

MAGNETOMETRE VECTORIELAFANAS'EV YU V; PRISHCHEPO VA; PORFIROV VP et al.PRISHCHEPO VA; 1977; IZMERITEL. TEKH.; S.S.S.R.; DA. 1977; NO 6; PP. 73-75; BIBL. 5 REF.Article

SOLID STATE THERMAL CONTROL FOR SPACECRAFT. = COMMANDE THERMIQUE A L'ETAT SOLIDE POUR VEHICULE SPATIALHARPSTER JWC; SWINEHART PR; BRAUN F et al.1975; SOLID-STATE ELECTRON.; G.B.; DA. 1975; VOL. 18; NO 6; PP. 551-555; BIBL. 8 REF.Article

MICROPARTICLE DETECTOR BASED ON THE ENERGY GAP DISAPPEARANCE OF SEMICONDUCTORS (SE, I, TE, BI, GE, SN, SI, AND INSB) AT HIGH PRESSURE.RAUSER P.1974; J. APPL. PHYS.; U.S.A.; DA. 1974; VOL. 45; NO 11; PP. 4869-4871; BIBL. 2 REF.Article

A MULTIWIRE PROPORTIONAL COUNTER WITH INTEGRAL READOUT DELAY LINEGILLAND JR; EMMING JG.1972; NUCL. INSTRUM. METHODS; NETHERL.; DA. 1972; VOL. 104; NO 1; PP. 241-243; BIBL. 3 REF.Serial Issue

SUCCESSFUL LARGE-SCALE USE OF CMOS DEVICES ON SPACECRAFT TRAVELING THROUGH INTENSE RADIATION BELTS.BRUCKER GJ; OHANIAN RS; STRASSINOPOULOS EG et al.1976; I.E.E.E. TRANS. AEROSPACE ELECTRON. SYST.; U.S.A.; DA. 1976; VOL. 12; NO 1; PP. 23-31; BIBL. 18 REF.Article

THERMOELECTRIC TEMPERATURE CONTROL OF INSTRUMENTATION. A SAMPLE DESIGN. = LES CAPTEURS DE TEMPERATURE THERMOELECTRIQUE POUR LA SURVEILLANCE DES APPAREILS. EXEMPLE DE CONCEPTIONMARTORANA RT.1975; I.E.E.E. TRANS. INDUSTR. ELECTRON. CONTROL INSTRUMENT.; U.S.A.; DA. 1975; VOL. 22; NO 1; PP. 69-75; BIBL. 3 REF.Article

ELECTRO-OPTICAL SYSTEMS.1975; AGARD-LS-76; FR.; DA. 1975; PP. (137P.); BIBL. DISSEM.Report

LA SIMULATION MATHEMATIQUE DES SYSTEMES D'ENERGIE.DUMONT A.1975; REV. H.F.; BELG.; DA. 1975; VOL. 9; NO 11; PP. 337-345Article

DATA SHEETS FOR PMC RADIOISOTOPIC FUELKEENAN TK; KENT RA; MULFORD RNR et al.1972; LA-4976-MS; U.S.A.; DA. 1972; PP. (8 P.); MICROFICHEReport

DESIGN POINT CHARACTERISTICS OF A 500-2500 WATT ISOTOPE-BRAYTON POWER SYSTEMBARNA GJ.sdIN: AM. INST. AERONAUT. ASTRONAUT. SOC. AUTOMOT. ENG. 8TH JOINT PROPUL. SPEC. CONF.; NEW ORLEANS, LA.; 1972; NEW YORK, N.Y.; A.I.A.A.; DA. S.D.; NO 1059; PP. 1-7; BIBL. 5 REF.Conference Paper

INTEGRATED CIRCUIT CHARACTERISTICS AT 260OC FOR AIRCRAFT ENGINE-CONTROL APPLICATIONSPALKUTI LJ; PRINCE JL; GLISTA AS JR et al.1979; I.E.E.E. TRANS. COMPON. HYBR. MANUFG TECHNOL.; USA; DA. 1979; VOL. 2; NO 4; PP. 405-412; BIBL. 8 REF.Article

IMPROVED TECHNOLOGY FOR MULTIWATT RADIOISOTOPE HEATER UNITSBARSELL AW; GORANSON RB; CLEMENTS PR et al.1973; NUCL. TECHNOL.; U.S.A.; DA. 1973; VOL. 19; NO 2; PP. 117-125; BIBL. 9 REF.Serial Issue

ELECTRONIQUE ASSOCIEEsdIN: PROPUL. ELECTR. APPL. SPAT. 2EME JOURN. ETUD. TOULOUSE, 1972; S.L.; DA. S.D.; PP. 237-308; ABS. ANGL.; BIBL. DISSEM.Conference Paper

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

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