Aluminum variable-conductive heat pipes of the communication satellites

Двирный, В В; Zagar, O.; Golovanov, Yu.; Ермилов, С П; Smirnov-Vasiliev, K.; Халиманович, В И; Lekanov, A. V.; Panov, G. E.; Ovechkin, G. V.; Kozlov, A.; Sinkovsky, F.

doi:10.1063/1.57672

Cited by 2 publications

(2 citation statements)

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“…The required inclination of the HP longitudinal axis is regulated by 3 supports (7), using the indicator of levelling (19). To minimize the thermal impact of the external temperature, the assembly is closed by thermal shield (17), having the same temperature as the mounting plate (6). The electrical heater is powered from the source of the regulated and stabilised voltage (12) and measured by a powermeter (11) or a combination of an ampere-meter and voltmeter.…”

Section: Objects For Studymentioning

confidence: 99%

“…The development of space thermal control technique is tightly connected with the achievements of heat pipe science and technology during the last 45 years [1][2][3][4][5][6]. As the main elements of TCS the different types of heat pipes are used: conventional heat pipes (HP), variable conductance (or resistance) heat pipes (VCHP), thermal diodes (TD), characteristics of which are described in Figure 1.…”

Section: Introductionmentioning

confidence: 99%

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Study of longitudinal heat transfer in low temperature heat pipes with axial grooves and discrete metal fibres for space thermal control systems

Baturkin¹,

Ho²

2016

Heat Transfer XIV: Simulation and Experiments in Heat Transfer and Its Applications

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Heat pipe technology became an integral part of the thermal control systems of space missions to transfer heat and control the temperature. The selection, design and the integration of heat pipes in space hardware requires the knowledge about their thermal performance. One of the major characteristics is the longitudinal resistance. This paper presents the experimental results of the longitudinal heat transfer in constant and variable thermal resistance heat pipes (HP) with diameters between 0.006 to 0.012 m: "a") aluminium -ammonia HP with axial grooved capillary structure; "b") stainless steel -methanol HP with stainless steel discrete metal fibre capillary structure; "c") copper -methanol HP with copper discrete metal fibre capillary structure. The tests have been performed within a wide range of operation parameters: heat sink temperature from -75 up to +60 o C, the transferred heat power from 0.5 up to 100 W, the axial heat flux density up to 250 W/cm 2 . As characteristic parameter the longitudinal thermal resistance R HP =(T ev -T con )/Q HP is used, where Q HP is the transferred heat power and T ev and T con are the average temperatures of the heat input and output zones, respectively. For the HPs "a" the parameter R HP varies from 0.06 to 0.045 K/W. The change of T con has no essential impact on the HP thermal resistance. For the HP "b", R HP changes from 80 to 4 K/W. The physical basis of such behaviour is related to the formation of vapor and non-condensable gas boundary in the coldest part of the heat pipe and, as consequence, a heat transfer intensity variation. The HPs "c" have shown essential impact of T con on resistance, which varies from 70 to 0.4 K/W. The physical basis of such behaviour is connected a change of the vapor flow regime in the inner vapor space and with change of the inner heat transfer intensity. The comparison of the longitudinal heat transfer characteristics of different types of heat pipes allows us to define their functional abilities in thermal control systems (TCS) for different space applications and to use these data in TCS mathematic models.

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Section: Objects For Studymentioning

confidence: 99%