发明名称 Active thermal load control system for spacecraft
摘要 The system has a storage tank (18) in which working fluid (52) is stored. Heating and cooling units (82,64) are coupled to the tank through a conduit assembly (30). The conduit assembly performs transition of heat between heating and cooling units by passage of fluid conveyed through the conduit.
申请公布号 DE19815941(A1) 申请公布日期 1998.12.17
申请号 DE19981015941 申请日期 1998.04.09
申请人 MOTOROLA, INC. (N.D.GES.D. STAATES DELAWARE), SCHAUMBURG, ILL., US 发明人 BASUTHAKUR, SIBNATH, PHOENIX, ARIZ., US;ALLEN, ROBERT D., TEMPE, ARIZ., US;MILLER, DANIEL D., SUPERIOR, COL., US
分类号 B64G1/40;B64G1/50;(IPC1-7):B64G1/50 主分类号 B64G1/40
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