TEST BENCH FOR SPACECRAFT RADIO ELECTRONIC THERMAL TESTS Russian patent published in 2015 - IPC B64G7/00 

Abstract RU 2553411 C1

FIELD: aircraft engineering.

SUBSTANCE: test bench comprises compact vacuum chamber with cryogenic shield and extra shield aligned therewith. Said extra shield is composed of high-heat-conductivity material with coating applied on its inner and outer surfaces that features a maximum degree of blackness. Besides, it incorporates an appliance (for example, a cold plate simulator) to fit test object inside said extra shield. Adjustable-capacity heaters are regularly arranged in circular space between both said shields. IR heaters can be arranged in vacuum chamber end section.

EFFECT: expanded range of tests, lower labour and time input, liquid nitrogen savings.

5 cl, 2 dwg

Similar patents RU2553411C1

Title Year Author Number
STAND FOR CONDUCTING THE SPACECRAFT HEAT AND VACUUM TESTS 2005
  • Sevast'Janov Nikolaj Nikolaevich
  • Verkhoturov Vladimir Ivanovich
  • Zjablov Valerij Arkad'Evich
  • Shcherbakov Ehduard Viktorovich
RU2302983C1
METHOD OF THERMAL-VACUUM TESTS OF SPACE VEHICLES AND DEVICE FOR ITS IMPLEMENTATION 2014
  • Kolchanov Igor' Petrovich
  • Ovechkin Gennadij Ivanovich
  • Kishkin Aleksandr Anatol'Evich
  • Sharov Aleksandr Konstantinovich
  • Ankudinov Aleksandr Vladimirovich
RU2565149C2
STAND FOR THERMAL VACUUM TESTING OF SPACECRAFT ELEMENTS 2020
  • Davidenko Dmitrij Valerevich
  • Zyablov Valerij Arkadevich
  • Kapustkin Dmitrij Petrovich
  • Shpikalov Leonid Vyacheslavovich
  • Shcherbakov Eduard Viktorovich
RU2759359C1
METHOD FOR OUTGASSING STRUCTURAL ELEMENTS OF SPACECRAFT IN GROUND CONDITIONS 2021
  • Davidenko Dmitrij Valerevich
  • Zyablov Valerij Arkadevich
  • Oksov Igor Andreevich
  • Trojnikov Vladimir Ivanovich
RU2778479C1
METHOD OF DETERMINING THERMAL RESISTANCE OF SPACECRAFT TEMPERATURE CONTROL VACUUM SHIELD THERMAL INSULATION SYSTEM FOR THERMAL-VACUUM TESTS 2006
  • Kornilov Vladimir Aleksandrovich
RU2355608C2
METHOD FOR SIMULATION OF EXTERNAL HEAT TRANSFER CONDITIONS OF SPACE VEHICLES IN THERMAL VACUUM CHAMBER 2023
  • Pastushenko Oleg Valerevich
  • Shevchuk Andrei Aleksandrovich
  • Dvirnyi Valerii Vasilevich
RU2801979C2
METHOD FOR SIMULATING EXTERNAL HEAT FLOWS FOR GROUND TESTING OF THERMAL CONDITIONS OF SPACECRAFT 2022
  • Davidenko Dmitrij Valerevich
  • Mashkova Nadezhda Vitalevna
  • Medvedev Vasilij Nikolaevich
RU2803298C1
METHOD OF HEAT-VACUUM TEST OF SPACECRAFT 2014
  • Grishko Mikhail Ivanovich
  • Smirnov Aleksandr Sergeevich
  • Pozhalov Vjacheslav Mikhajlovich
  • Mitrofanov Mikhail Sergeevich
RU2564056C1
DEVICE FOR GRADUATING RADIANT ENERGY RECEIVERS 2009
  • Kornilov Vladimir Aleksandrovich
RU2408854C1
METHOD OF THERMAL VACUUM TESTS AND DEVICE FOR REALIZATION OF THIS METHOD 2001
  • Zelenov I.A.
  • Nikitin P.V.
  • Shabarchin D.A.
  • Mitrofanov V.F.
  • Ozerov L.A.
RU2208564C1

RU 2 553 411 C1

Authors

Egorov Konstantin Vladilenovich

Alekseev Vladimir Antonovich

Kopylov Viktor Zakharovich

Karaban Leonid Vasil'Evich

Dates

2015-06-10Published

2014-01-28Filed