SPACECRAFT Russian patent published in 2000 - IPC

Abstract RU 2144889 C1

FIELD: space engineering; designing of spacecraft. SUBSTANCE: spacecraft includes compartments with target and service equipment, storage battery power supply system (in equipment compartment) and temperature control system which is provided with devices for taking, supplying and removing heat; some of them are made in form of thermal plates with hydraulic passages. Thermal plate forming monoblock unit with battery is secured on bottom of each battery. Monoblock unit is secured in equipment compartment by means of units made in housing of each battery. Thermal plate of each monoblock is provided with additional hydraulic passages interconnected by means of pipe lines. These passages and lines form independent open main. EFFECT: facilitated procedure of ground tests of spacecraft; limited assembly jobs on spacecraft; improved service life characteristics of spacecraft power supply and temperature control system. 2 dwg

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RU 2 144 889 C1

Authors

Gurtov A.S.

Filatov A.N.

Fomakin V.N.

Tomina V.S.

Kitaev A.I.

Bykov S.M.

Dates

2000-01-27—Published

1998-10-26—Filed