Pascal and Francis Bibliographic Databases

Help

Search results

Your search

kw.\*:("CALODUC THERMOSTAT")

Document Type [dt]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Publication Year[py]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Discipline (document) [di]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Language

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Author Country

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Results 1 to 25 of 80

  • Page / 4
Export

Selection :

  • and

EVALUATION OF A LARGE SIZE MODULAR HEAT PIPE/RADIATOR FOR CRYOGENIC THERMAL CONTROL = ETUDE DES CARACTERISTIQUES D'UN CALODUC/RADIATEUR MODULAIRE DE GRANDE DIMENSION POUR LE CONTROLE THERMIQUE CRYOGENIQUENELSON BE; PETRIE W.1974; IN: AM. SOC. MECH. ENG. INTERSOC. CONF. ENVIRON. SYST.; SEATTLE; 1974; NEW YORK; A.S.M.E.; DA. 1974; VOL. 29; PP. 1-8; BIBL. 9 REF.Conference Paper

ANALYSIS AND TESTING OF A HEAT PIPE MIRROR FOR LASERS. = ANALYSE ET ESSAIS D'UN CALODUC POUR MIROIR DE LASERJACOBSON DL; BICKFORD W; KIDD J et al.1975; IN: AM. INST. AERONAUT. ASTRONAUT. 10TH THERMOPHYS. CONF.; DENVER, COLO.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 655; PP. 1-10; BIBL. 5 REF.Conference Paper

HEAT PIPE THERMAL CONTROL OF IRRADIATION CAPSULES = CONTROLE THERMIQUE PAR CALODUC DES CAPSULES D'IRRADIATIONDEVERALL JE.sdIN: INT. HEAT PIPE CONF.; PREPR. STUTTGART; 1973; DUESSELDORF; VER. DTSCH. ING.; DA. S.D.; PP. 1-11; BIBL. 3 REF.Conference Paper

A VARIABLE CONDUCTANCE HEAT PIPE FLIGHT EXPERIMENT: PERFORMANCE IN SPACE. = UN CALODUC THERMOSTAT: ESSAI ET PERFORMANCE EN VOLWANOUS DJ; MARCUS BD; KIRKPATRICK JP et al.1975; IN: AM. INST. AERONAUT. ASTRONAUT. 10TH THERMOPHYS. CONF.; DENVER, COLO.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 655; PP. 1-7; BIBL. 5 REF.Conference Paper

HEAT PIPE THERMAL CONDITIONING PANEL = PANNEAU CONDITIONNE THERMIQUEMENT PAR CALODUCSAASKI EW; LOOSE JD; MCCOY KE et al.1974; IN: AM. SOC. MECH. ENG. INTERSOC. CONF. ENVIRON. SYST.; SEATTLE; 1974; NEW YORK; A.S.M.E.; DA. 1974; VOL. 37; PP. 1-8Conference Paper

SPACE SHUTTLE HEAT PIPE THERMAL CONTROL SYSTEMS; DESIGN AND TEST = SYSTEMES CONDITIONNES THERMIQUEMENT PAR CALODUC POUR DES MISSIONS SPATIALES ALLER-RETOUR; CONCEPTION ET ESSAISALARIO J.1974; IN: AM. SOC. MECH. ENG. INTERSOC. CONF. ENVIRON. SYST.; SEATTLE; 1974; NEW YORK; A.S.M.E.; DA. 1974; VOL. 38; PP. 1-12; BIBL. 7 REF.Conference Paper

ADVANCED THERMAL CONTROL FLIGHT EXPERIMENT = CONTROLE THERMIQUE EN VOL; TECHNIQUE AVANCEE ET EXPERIENCEKIRKPATRICK JP; BRENNAN PJ.1974; PROGR. ASTRONAUT. AERONAUT.; U.S.A.; DA. 1974; VOL. 35; PP. 409-430; BIBL. 9 REF.; (THERMOPHYS. SPACECR. THERM. CONTROL. AIAA 8 TH THERMOPHYS. CONF. TECH. SEL. PAP.; PALM SPRINGS, CALIF.; 1973)Conference Paper

HEAT PIPES WITH HEADER AND ARTERY SYSTEMSCHISHOLM D.1978; INTERNATION. J. HEAT MASS TRANSFER; GBR; DA. 1978; VOL. 21; NO 9; PP. 1207-1212; ABS. FRE/GER/RUS; BIBL. 5 REF.Article

CONTROLLABILITY ANALYSIS FOR PASSIVELY AND ACTIVELY CONTROLLED HEAT PIPES.LEHTINEN AM.1977; IN: AM. INST. AERONAUT. ASTRONAUT. THERMOPHYS. CONF. 12; ALBUQUERQUE; N. MEX.; 1977; NEW YORK; AIAA; DA. 1977; VOL. 726; PP. (12P.); BIBL. 3 REF.Conference Paper

WAERMEROHR ZUR AUSNUETZUNG DER WAERMEKAPAZITAET VON ERDREICH = HEAT PIPE FOR GROUND THERMAL CONTROL = CALODUCS POUR L'UTILISATION DE LA CAPACITE THERMIQUE DU SOLBSCHORR O.1981; BRENNSTOFF-WAERME-KRAFT; ISSN 0006-9612; DEU; DA. 1981; VOL. 33; NO 12; PP. 490-491; BIBL. 7 REF.Article

A VARIABLE CONDUCTANCE HEAT PIPE USING BUBBLE PUMP INJECTION.ROBERTS CC JR.sdIN: INT. HEAT PIPE CONF. 2. PREPR.; BOLOGNA; 1976; NOORDWIJK, NETH.; EUR. SPACE AGENCY; DA. S.D.; VOL. 1; PP. 269-280; BIBL. 3 REF.Conference Paper

STUDY OF THERMOSTABILITY CHARACTERISTICS IN SOLUBLE GAS CONTROLLED HEAT PIPESSEMENA MG; MYULLER R.1980; TEPLOFIZ. VYS. TEMP.; ISSN 0040-3644; SUN; DA. 1980; VOL. 18; NO 4; PP. 846-851; BIBL. 8 REF.Article

AN ACTIVELY CONTROLLED HEAT PIPE CALCULATIONVASIL'EV LL; TOMCHAK V; KONEV SV et al.1979; INZHENER.-FIZ. ZH.; BYS; DA. 1979; VOL. 37; NO 1; PP. 20-26; ABS. ENG; BIBL. 5 REF.Article

A ZERO-G VARIABLE CONDUCTANCE HEAT PIPE USING BUBBLE PUMP INJECTION.ROBERTS CC.1977; IN: AM. INST. AERONAUT. ASTRONAUT. THERMOPHYS. CONF. 12; ALBUQUERQUE, N. MEX.; 1977; NEW YORK; AIAA; DA. 1977; VOL. 726; PP. (10P.); BIBL. 5 REF.Conference Paper

DEVELOPMENT OF VAPOR-FLOW-MODULATION VARIABLE CONDUCTANCE HEAT PIPES.MARCUS BD; ENINGER JE.sdIN: INT. HEAT PIPE CONF. 2. PREPR.; BOLOGNA; 1976; NOORDWIJK, NETH.; EUR. SPACE AGENCY; DA. S.D.; VOL. 1; PP. 257-268; BIBL. 10 REF.Conference Paper

DAS WAERMEROHR - EIN NEUARTIGES BAUTEIL HOECHSTER WAERMELEITFAEHIGKEIT. = THE HEAT PUMP. A NEW VERY HIGH THERMAL CONDUCTIVITY COMPONENT = LE CALODUC. UN NOUVEAU COMPOSANT D'UNE TRES GRANDE CONDUCTIVITE THERMIQUEBAUMULLER K; HASCHKE M; KERSTIN L et al.1978; TECHNIK; DTSCH.; DA. 1978; VOL. 33; NO 5; PP. 259-261; ABS. RUSSE ANGL. FR.; BIBL. 15 REF.Article

A VARIABLE CONDUCTANCE HEAT PIPE FOR TERRESTRIAL APPLICATIONSMOLT W.1978; INTERNATIONAL HEAT PIPE CONFERENCE. 3/1978/PALO ALTO CA; USA; DA. 1978; PP. 10-14; BIBL. 5 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

STUDY OF VARIABLE OR CONSTANT RESERVOIR NON CONDENSIBLE GAS CONTROLLED HEAT PIPESBARSUKOV VV.1976; INZHENER.-FIZ. ZH., BELORUS. S.S.R.; S.S.S.R.; DA. 1976; VOL. 31; NO 4; PP. 587-593; ABS. ANGL.; BIBL. 5 REF.Article

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

FONDAMENTALS OF THE TEMPERATURE STABILIZATION PROCESS IN VARIABLE CONDUCTANCE HEAT PIPESVASIL'EV LL; KONEV SV.1978; INZHENER.-FIZ. ZH., BELORUS. S.S.R.; S.S.S.R.; DA. 1978; VOL. 34; NO 5; PP. 776-784; ABS. ANGL.; BIBL. 9 REF.Article

BREVET DISPOSITIF DE TRANSFERT DE CHALEUR1978; ; FRA; DA. 1978-09-22; FR/A1/2.378.248; DEP.77-01446/1977-01-19Patent

STEADY-STATE AND START UP CARACTERISTICS OF A HEAT PIPE WITH WICKLESS RESERVOIRSEMENA MG; BATURKIN VM; RASSAMAKIN BM et al.1977; INZHENER.-FIZ. ZH., BELORUS. S.S.R.; S.S.S.R.; DA. 1977; VOL. 33; NO 3; PP. 381-387; ABS. ANGL.; BIBL. 6 REF.Article

STAND DER ENTWICKLUNG UND ANWENDUNG VON GASSTABILISIERTEN HEAT- PIPE- RADIATOREN. = STATUS AND USE OF VARIABLE CONDUCTANCE HEAT PIPE RADIATORS = SITUATION DU DEVELOPPEMENT ET DE L'UTILISATION DES RADIATEURS-CALODUCS A GAZ STABILISEKOCH H.1976; JB. DTSCH. GESSELLSCH. LUFT-U. RAUMFAHRT; DTSCH.; DA. 1976; VOL. 4; NO 192.1-192.27; BIBL. 4 REF.Article

TRANSVERSE HEADER HEAT PIPE. = CALODUC A TETE DE TUBE TRANSVERSALEEDELSTEIN F.1975; IN: AM. INST. AERONAUT. ASTRONAUT. 10TH THERMOPHYS. CONF.; DENVER, COLO.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 655; PP. 1-7; BIBL. 9 REF.Conference Paper

  • Page / 4