METHOD OF OPERATION OF SPACECRAFT THERMAL CONTROL SYSTEM SIMULATOR Russian patent published in 2015 - IPC B64G7/00 B64G1/50 

Abstract RU 2541612 C2

FIELD: test equipment.

SUBSTANCE: invention refers mainly to land tests and drills of spacecraft thermal control system. According to invention, heat carrier deficiency in the system of thermal control system simulator and payload module is determined in advance. For that purpose, heat carrier temperature is measured regularly in fluid paths of the simulator and payload module before payload module test. Gas pressure in gas cavity of pressuriser of thermal control system simulator is measured at mean measured temperature below temperature of heat carrier and gas loading to the simulator. The pressure is compared to acceptable minimum value determined by a certain relation. If the pressure measured is below acceptable minimum then a heat carrier amount missing is added to the simulator fluid path from separate small compensation device.

EFFECT: improved long-term operation reliability of thermal control system simulator.

6 dwg

Similar patents RU2541612C2

Title Year Author Number
METHOD OF MANUFACTURE OF PAYLOAD MODULE FOR SPACECRAFT 2003
  • Kozlov Al'Bert Gavrilovich
  • Bartenev Vladimir Afanas'Evich
  • Kesel'Man Gennadij Davydovich
  • Shelud'Ko Vjacheslav Grigor'Evich
  • Khalimanovich Vladimir Ivanovich
  • Mikhnev Mikhail Mikhajlovich
  • Akchurin Vladimir Petrovich
  • Akchurin Georgij Vladimirovich
  • Bliznevskij Aleksandr Sergeevich
  • Roskin Sergej Mikhajlovich
  • Golovenkin Evgenij Nikolaevich
  • Turkenich Roman Petrovich
  • Gupalo Viktor Kuz'Mich
  • Zagar Oleg Vjacheslavovich
  • Shilkin Oleg Valentinovich
  • Dmitriev Gennadij Valer'Evich
RU2269457C2
TEST METHOD OF SPACECRAFT TEMPERATURE CONTROL SYSTEM 2018
  • Kolesnikov Anatolij Petrovich
  • Legostaj Igor Vasilevich
  • Shilkin Oleg Valentinovich
  • Akchurin Vladimir Petrovich
  • Dmitriev Gennadij Valerevich
  • Marchenko Igor Anatolevich
  • Svinin Timofej Petrovich
  • Ovchinnikov Konstantin Vasilevich
  • Bakurov Evgenij Yurevich
  • Sokolov Sergej Nikolaevich
RU2698573C1
SPACECRAFT TEMPERATURE CONTROL SYSTEM 2005
  • Kozlov Al'Bert Gavrilovich
  • Bartenev Vladimir Afanas'Evich
  • Shelud'Ko Vjacheslav Grigor'Evich
  • Khalimanovich Vladimir Ivanovich
  • Akchurin Vladimir Petrovich
  • Bliznevskij Aleksandr Sergeevich
  • Golovenkin Evgenij Nikolaevich
  • Dedjulin Aleksandr Leonidovich
  • Zagar Oleg Vjacheslavovich
  • Nikitin Vladislav Nikolaevich
  • Popov Vasilij Vladimirovich
  • Roskin Sergej Mikhajlovich
  • Sergeev Jurij Dmitrievich
  • Tomchuk Al'Bert Vladimirovich
  • Turkenich Roman Petrovich
  • Shilkin Oleg Valentinovich
RU2288143C2
COMMUNICATION SATELLITE TEMPERATURE CONTROL SYSTEM 1999
  • Akchurin V.P.
  • Bartenev V.A.
  • Zagar O.V.
  • Kozlov A.G.
  • Korchagin E.N.
  • Lekanov A.V.
  • Talabuev E.S.
  • Tomchuk A.V.
  • Turkenich R.P.
  • Khalimanovich V.I.
  • Shilkin O.V.
RU2158703C1
METHOD OF TESTING SPACECRAFT AND DEVICE FOR REALIZATION OF THIS METHOD 2000
  • Akchurin V.P.
  • Bartenev V.A.
  • Golovenkin E.N.
  • Zagar O.V.
  • Kozlov A.G.
  • Korchagin E.N.
  • Tomchuk A.V.
  • Turkenich R.P.
  • Khalimanovich V.I.
  • Shilkin O.V.
RU2200689C2
METHOD OF FILLING LIQUID LOOP OF TEMPERATURE CONTROL SYSTEM WITH HEAT-TRANSFER AGENT AND DEVICE FOR REALIZATION OF THIS METHOD 2003
  • Kozlov Al'Bert Gavrilovich
  • Bartenev Vladimir Afanas'Evich
  • Kesel'Man Gennadij Davydovich
  • Shelud'Ko Vjacheslav Grigor'Evich
  • Khalimanovich Vladimir Ivanovich
  • Mikhnev Mikhail Mikhajlovich
  • Akchurin Vladimir Petrovich
  • Bliznevskij Aleksandr Sergeevich
  • Roskin Sergej Mikhajlovich
  • Golovenkin Evgenij Nikolaevich
  • Turkenich Roman Petrovich
  • Zagar Oleg Vjacheslavovich
  • Shilkin Oleg Valentinovich
  • Dmitriev Gennadij Valer'Evich
  • Golovanov Jurij Matveevich
RU2269461C2
SPACECRAFT TEMPERATURE CONTROL SYSTEM AND METHOD OF ITS MANUFACTURE 2000
  • Akchurin V.P.
  • Bartenev V.A.
  • Zagar O.V.
  • Kozlov A.G.
  • Talabuev E.S.
  • Tomchuk A.V.
  • Turkenich R.P.
  • Khalimanovich V.I.
  • Shilkin O.V.
RU2191359C2
METHOD OF CONSTRUCTING SPACECRAFT 2013
  • Testoedov Nikolaj Alekseevich
  • Kosenko Viktor Evgen'Evich
  • Khalimanovich Vladimir Ivanovich
  • Golovenkin Evgenij Nikolaevich
  • Popov Vasilij Vladimirovich
  • Sorokvasha Gennadij Grigor'Evich
  • Kolesnikov Anatolij Petrovich
  • Ankudinov Aleksandr Vladimirovich
  • Akchurin Georgij Vladimirovich
  • Dostavalov Aleksandr Valentinovich
  • Vilkov Jurij Vjacheslavovich
  • Kuvakin Konstantin Leonardovich
  • Shilkin Oleg Valentinovich
  • Akchurin Vladimir Petrovich
RU2541598C2
METHOD FOR CONTROL OF HEAT CARRIER AMOUNT IN LIQUID CHANNEL OF SPACE VEHICLE THERMAL CONTROL 2009
  • Khalimanovich Vladimir Ivanovich
  • Zagar Oleg Vjacheslavovich
  • Lekanov Anatolij Vasil'Evich
  • Kolesnikov Anatolij Petrovich
  • Akchurin Georgij Vladimirovich
  • Sinichenko Mikhail Ivanovich
  • Shilkin Oleg Valentinovich
  • Akchurin Vladimir Petrovich
  • Nikitin Vladislav Nikolaevich
RU2404089C1
METHOD OF TESTING SPACECRAFT AND DEVICE FOR REALIZATION OF THIS METHOD 2001
  • Akchurin V.P.
  • Bartenev V.A.
  • Bliznevskij A.S.
  • Golovenkin E.N.
  • Zagar O.V.
  • Kozlov A.G.
  • Korchagin E.N.
  • Popov V.V.
  • Roskin S.M.
  • Talabuev E.S.
  • Tomchuk A.V.
  • Turkenich R.P.
  • Khalimanovich V.I.
  • Shilkin O.V.
RU2209751C2

RU 2 541 612 C2

Authors

Khalimanovich Vladimir Ivanovich

Golovenkin Evgenij Nikolaevich

Sorokvasha Gennadij Grigor'Evich

Kolesnikov Anatolij Petrovich

Ankudinov Aleksandr Vladimirovich

Akchurin Georgij Vladimirovich

Volovikov Vitalij Gavriilovich

Shilkin Oleg Valentinovich

Akchurin Vladimir Petrovich

Urakov Sergej Andreevich

Dates

2015-02-20Published

2013-04-17Filed