Increasingly stringent thermal requirements are projected for future spacecraft. Compliance with these requirements necessitates the development of two-phase thermal control loops. These systems require a heat exchanger to couple the condenser section of the loop to a heat pipe radiator assembly. This paper presents a preliminary design of such a heat exchanger.
A low pressure drop heat exchanger with integral heat pipe
Niederdruck-Tropfenwaermetauscher mit integralem Waermerohr
ASME Proc. of the 1988 Nat. Heat Transfer Conf. ; HTD-96 , Jul ; 367-377
1988
11 Seiten, 10 Bilder, 1 Tabelle, 10 Quellen
Conference paper
English
Modular Heat Exchanger With Integral Heat Pipe
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