PERIODE INITIALE DE DEVELOPPEMENT DE SPATIONAUTIQUE EN URSS (1917-1945)TOLMACHEV EP.1982; KOSM. BIOL. AVIAKOSM. MED.; ISSN 0321-5040; SUN; DA. 1982; VOL. 16; NO 6; PP. 7-15; BIBL. 31 REF.Article

HEAT PIPES FOR SPACE USE.ACCENSI A; SAVAGE CJ.1977; E.S.A. BULL.; FRA; DA. 1977; NO 10; PP. 49-55Article

ENERGY IMPACT ASSESSMENT OF NASA'S PAST, PRESENT, AND FUTURE SPACE LAUNCH VEHICLESRICE EE.1978; J. ENERGY; USA; DA. 1978; VOL. 2; NO 3; PP. 182-188; BIBL. 20 REF.Article

ENTWICKLUNGEN DER LUFT- UND RAUMFAHRT FUER DIE DEZENTRALE ENERGIEVERSORGUNG. ELEKTRISCHE ENERGIEVERSORGUNG MIT REGENERATIVEN ENERGIEQUELLEN = CONTRIBUTION DE L'AERONAUTIQUE ET DE L'AEROSPATIALE A L'APPROVISIONNEMENT AUTONOME EN ENERGIE. APPROVISIONNEMENT EN ENERGIE ELECTRIQUE A PARTIR DE SOURCES RENOUVELABLESKOETHE HK.1982; VDI-BERICHTE; ISSN 0083-5560; DEU; DA. 1982; NO 455; PP. 85-89Article

HEAT PIPE COOLING OF AN AEROSPACE FOAM MOLD MANUFACTURING PROCESSFELDMANN KT; MARJON PL; HAHN DR et al.1980; AEROSPACE SCIENCES MEETING. 18/1980/PASADENA CA; USA; NEW YORK: AIAA; DA. 1980; 6 P.; BIBL. 1 REF.Conference Paper

THE INTERNATIONAL HEAT PIPE EXPERIMENT.HARWELL W; MCINTOSH R; OLLENDORF S et al.sdIN: INT. HEAT PIPE CONF. 2. PREPR.; BOLOGNA, ITALY; 1976; NOORDWIJK, NETH.; EUR. SPACE AGENCY; DA. S.D.; VOL. 1; PP. 589-591Conference Paper

DEVELOPMENT OF A FACTOR COMPRESSION HEAT PUMP FOR SPACE USEBERNER F; SAVAGE CJ.1981; THERMOPHYSICS CONFERENCE. 16/1981-06-23/PALO ALTO CA; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 81-1113; 11 P.; BIBL. 5 REF.Conference Paper

PERFORMANCE TESTING OF A HYDROGEN HEAT PIPEALARIO J; KOSSON R.1980; AEROSPACE SCIENCES MEETING. 18/1980/PASADENA CA; USA; NEW YORK: AIAA; DA. 1980; 8 P.; BIBL. 2 REF.Conference Paper

A PRECISE SATELLITE THERMAL CONTROL SYSTEM USING CASCADED HEAT PIPES.MCKEE HB; STEELE WH.1977; IN: AM. INST. AERONAUT. ASTRONAUT. THERMOPHYS. CONF. 12; ALBUQUERQUE, N. MEX.; 1977; NEW YORK; AIAA; DA. 1977; VOL. 726; PP. (11P.); BIBL. 6 REF.Conference Paper

THE INTERNATIONAL HEAT PIPE EXPERIMENT.MCINTOSH R; OLLENDORF S; SHERMAN A et al.sdIN: INT. HEAT PIPE CONF. 2. PROC.; BOLOGNA; 1976; NOORDWIJK, NETH.; ESA SCI. TECH.; DA. S.D.; PP. 815-837; BIBL. 13 REF.Conference Paper

CRYOGENIC AND LOW-TEMPERATURE HEAT PIPE/COOLER STUDIES FOR SPACECRAFT APPLICATION.SHERMAN A; BRENNAN P.1976; J. SPACECR. ROCK.; U.S.A.; DA. 1976; VOL. 13; NO 5; PP. 288-293; BIBL. 8 REF.Article

DEFINITION OF A CRYOGENIC HEAT PIPE EXPERIMENT.KROLICZEK EJ.sdIN: INT. HEAT PIPE CONF. 2. PREPR.; BOLOGNA, ITALY; 1976; NOORDWIJK, NETH.; EUR. SPACE AGENCY; DA. S.D.; VOL. 1; PP. 673-682Conference Paper

DESIGN AND EVALUATION OF A ROTATING VARIABLE CONDUCTANCE HEAT PIPE SYSTEMMARSHBURN JP; MCINTOSH R JR.1978; INTERNATIONAL HEAT PIPE CONFERENCE. 3/1978/PALO ALTO CA; USA; DA. 1978; PP. 211-215Conference Paper

DEVELOPMENT OF AN AXIALLY GROOVED HEAT PIPE WITH NON-CONSTANT GROOVE WIDTHSCHLITT KR.1978; INTERNATIONAL HEAT PIPE CONFERENCE. 3/1978/PALO ALTO CA; USA; DA. 1978; PP. 1-9; BIBL. 7 REF.Conference Paper

SATELLITE BATTERY TEMPERATURE CONTROLEDELSTEIN F; FLIEGER H.1978; INTERNATIONAL HEAT PIPE CONFERENCE. 3/1978/PALO ALTO CA; USA; DA. 1978; PP. 360-366Conference Paper

BREVET DISPOSITIF ASSURANT LE DEGAZAGE D'UN LIQUIDE PARCOURANT DES TUBES DE TRANSMISSION DE CHALEUR1978; ; FRA; DA. 1978-10-13; FR/A1/2.380.520; DEP.77 39960/1977-12-28; PR. DE/P 2705457.5/1977-02-10Patent

A PRECISE SATELLITE THERMAL CONTROL SYSTEM USING CASCADED HEAT PIPESSTEELE WH; MCKEE HB.1978; PROGR. ASTRONAUT. AERONAUT.; USA; DA. 1978; VOL. 60; PP. 325-343; BIBL. 6 REF.Article

SPACE CONDITIONS EXPERIMENTS FOR A HEAT PIPEVASIL'EV LL; GIL VV; ZHARIKOV NA et al.1976; INZHENER.-FIZ. ZH., BELORUS. S.S.R.; S.S.S.R.; DA. 1976; VOL. 31; NO 6; PP. 990-995; ABS. ANGL.; BIBL. 6 REF.Article

THE CHARACTERIZATION OF A GRAVITY ASSISTED HEAT PIPE WITH INTERNAL TWO PHASE PARALLEL FLOW THROUGHOUTCUNDY VA; HA LN.1982; SOUTHEASTERN SEMINAR ON THERMAL SCIENCES. 16/1981-04-19/MIAMI FL; USA; CORAL GABLES: CLEAN ENERGY RESEARCH INSTITUTE; DA. 1982; PP. 68Conference Paper

REACTOR DESIGN FOR NUCLEAR ELECTRIC PROPULSIONKOENIG DR; RANKEN WA.1979; INTERSOCIETY ENERGY CONVERSION ENGINEERING CONFERENCE. 14/1979/BOSTON MA; USA; WASHINGTON: AMERICAN CHEMICAL SOCIETY; DA. 1979; PP. 1418-1424; BIBL. 5 REF.Conference Paper

MODULAR HEAT PIPE RADIATORALARIO J; CANARAS T.1978; INTERSOCIETY CONFERENCE ON ENVIRONMENTAL SYSTEMS/1977/SAN FRANCISCO CA; USA; NEW YORK: ASME; DA. 1978; 11 P.Conference Paper

LONG TERM PERFORMANCE OF THE ADVANCED THERMAL CONTROL FLIGHT EXPERIMENT.BRENNAN PJ; KIRKPATRICK JP.sdIN: INT. HEAT PIPE CONF. 2. PREPR.; BOLOGNA, ITALY; 1976; NOORDWIJK, NETH.; EUR. SPACE AGENCY; DA. S.D.; VOL. 1; PP. 629-643; BIBL. 5 REF.Conference Paper

DESIGN AND DEVELOPMENT OF INTEGRAL HEAT PIPE/THERMAL ENERGY STORAGE DEVICESMAHEFKEY ET; RICHTER R.1981; THERMOPHYSICS CONFERENCE. 16/1981-06-23/PALO ALTO CA; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; AIAA-81-1159; 6 P.; BIBL. 6 REF.Conference Paper

THE CASCADED VARIABLE CONDUCTANCE HEAT PIPE EXPERIMENT FOR LDEFCALHOUN LD; GROTE MG.1981; THERMOPHYSICS CONFERENCE. 16/1981-06-23/PALO ALTO CA; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; AIAA-81-1157; 8 P.; BIBL. 3 REF.Conference Paper

THE ESA HEAT PIPE EXPERIMENT ON ASTRO-8(II)SAVAGE CJ; AALDERS BGM; MATHIEU JP et al.1979; THERMOPHYSICS CONFERENCE. 14/1979/ORLANDO FL; USA; NEW YORK: AIAA; DA. 1979; 79-1063; 6 P.; BIBL. 6 REF.Conference Paper