METHOD OF ASSEMBLING SPACECRAFT

• Main Authors: TESTOEDOV NIKOLAJ ALEKSEEVICH, AKCHURIN VLADIMIR PETROVICH, KUVAKIN KONSTANTIN LEONARDOVICH, KOLESNIKOV ANATOLIJ PETROVICH, BLIZNEVSKIJ ALEKSANDR SERGEEVICH, POPOV VASILIJ VLADIMIROVICH, TURKENICH ROMAN PETROVICH, BARTENEV VLADIMIR AFANAS'EVICH, JUROVSKIKH ANDREJ PETROVICH, GOLOVANOV JURIJ MATVEEVICH, KUZNETSOV ANATOLIJ JUR'EVICH, KHALIMANOVICH VLADIMIR IVANOVICH, KOSENKO VIKTOR EVGEN'EVICH, ZAGAR OLEG VJACHESLAVOVICH, SERGEEV JURIJ DMITRIEVICH, BASYNIN VIKTOR VLADIMIROVICH, KESEL'MAN GENNADIJ DAVYDOVICH, TOMCHUK AL'BERT VLADIMIROVICH, SHILKIN OLEG VALENTINOVICH
• Format: Patent
• Language: English; Russian
• Published: 20.02.2009
• Subjects: AIRCRAFT; AVIATION; COSMONAUTICS; PERFORMING OPERATIONS; TRANSPORTING; VEHICLES OR EQUIPMENT THEREFOR

FIELD: transportation. ^ SUBSTANCE: satellite consists of two modules: payload module and support system module, and their devices are fitted on honeycomb panels with built-in channels for circulating heat carrier under the devices. Radiators, with channels for circulating heat carrier, are placed in perpendicular planes to the axis +Z (-Z) of the spacecraft. Most of the devices of the payload module are fitted on extra panels with built-in channels for circulating heat carrier by putting them inside the provided free space between panels of the support system module. Opening-up extra radiator panels with built-in channels on the section of raising the spacecraft to the working orbit are folded parallel to the panels of the support system module, placed in planes perpendicular to the axis Y (-Y) of the spacecraft. ^ EFFECT: more reliable operation of devices of a spacecraft. ^ 2 cl, 6 dwg