COMMUNICATION SATELLITE TEMPERATURE CONTROL SYSTEM

space engineering; communication satellite temperature control systems. SUBSTANCE: proposed system includes heat exchangers, compensator, electric pumping unit and liquid loop with flow regulator and distributor. Distributor has one inlet and two outlets. Second outlet of distributor is connected wi...

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Bibliographische Detailangaben
Hauptverfasser:	KHALIMANOVICH V.I, SHILKIN O.V, KOZLOV A.G, ZAGAR O.V, BARTENEV V.A, LEKANOV A.V, TOMCHUK A.V, KORCHAGIN E.N, TALABUEV E.S, TURKENICH R.P, AKCHURIN V.P
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT AVIATION COSMONAUTICS PERFORMING OPERATIONS TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR
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Beschreibung
Zusammenfassung:	space engineering; communication satellite temperature control systems. SUBSTANCE: proposed system includes heat exchangers, compensator, electric pumping unit and liquid loop with flow regulator and distributor. Distributor has one inlet and two outlets. Second outlet of distributor is connected with outlet of radiator-cooler by means of bypass. Parameters of line from first outlet of distributor to point of connection with bypass satisfies special condition. Repeater cooling liquid passage is connected to system before testing the satellite through hydraulic connectors. To this end, hydraulic connectors are coupled together via circular partition provided with specially selected number of holes. EFFECT: enhanced reliability; increased service life of system; reduced mass; low-cost. 2 cl, 4 dwg