FIELD: heating.
SUBSTANCE: invention relates to heat accumulating devices using latent heat of phase transitions of working substance to provide required heat mode of energy sources during their cyclic operation. Disclosed is a radiator-heat accumulator of a passive thermal control system of a space object (SO), which operates in a periodic mode, and comprising a heat-removing base, a heat accumulator with a housing and an inner volume V with a heat accumulating substance and cooling channels. Housing of heat accumulator is made in form of radiation panel with thickness δ much smaller than characteristic size of its surface of heat radiation area F, and heat accumulating substance is uniformly distributed in continuous matrix phase with volume fraction εmp, contacting inner surface of housing and heat accumulating substance with density ρand mass M, with melting point Tm, and evenly distributed over the volume V coolant condensation zone with a volume fraction εchp controlled heat pipe and the melting point Tmwarm coolant, where on the heat-removing base of the SO there are electric heaters and a zone of evaporation of the controlled heat pipe, which maintain the temperature of SO Tso in the range of Tsomin...Tsomax. SO periodically operates in active mode with duration of τg with constantly allocated thermal power Wso and in standby mode with duration of τ0, wherein the required mass of heat-accumulating substance is evaluated from: M = Wso⋅τg/(c⋅ΔT⋅k1 + r⋅k2), where k1 = 1 + ε⋅σ⋅F⋅(Tx4 + 2⋅Tx3 ⋅ΔT + 2⋅Tx2⋅ΔT 2 + Tx⋅ΔT3 + 0.2⋅ΔT4)/Wso, k2 = 1 + ε⋅σ⋅F⋅Tpl4/Wso; r is specific heat of fusion of heat accumulating substance; ε – degree of radiation panel heat radiation surface blackness; σ is Stefan-Boltzmann constant; c is specific heat capacity of heat accumulating substance; ΔT = Tm – Tx, provided that Tx > Tmwarm, where Tx – temperature heat accumulating substance in the solid initial state, wherein internal volume of heat accumulator V corresponds to relationship: V = M/[ρ⋅(1 – εchp – εmp)], and the minimal necessary heat radiation surface of the radiation panel satisfies Fmin = M⋅r/(τ0⋅ε⋅σ⋅Tm4).
EFFECT: technical result is providing a compact design, high reliability and broader functional capabilities of the thermal control system.
10 cl, 4 dwg
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Authors
Dates
2020-03-13—Published
2019-04-11—Filed