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Thermo-vacuum test chamber development for airborne and space equipment testing in simulated extreme conditions

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F18%3APU129810" target="_blank" >RIV/00216305:26210/18:PU129810 - isvavai.cz</a>

  • Result on the web

    <a href="http://www.icas.org/ICAS_ARCHIVE/ICAS2018/data/papers/ICAS2018_0548_paper.pdf" target="_blank" >http://www.icas.org/ICAS_ARCHIVE/ICAS2018/data/papers/ICAS2018_0548_paper.pdf</a>

  • DOI - Digital Object Identifier

Alternative languages

  • Result language

    angličtina

  • Original language name

    Thermo-vacuum test chamber development for airborne and space equipment testing in simulated extreme conditions

  • Original language description

    The Institute of Aerospace Engineering, Brno University of Technology developed a unique thermo-vacuum test facility to simulate extreme aerospace environmental conditions. Even though originally developed for space technology Qualification tests, the know-how can be used to test airborne equipment in laboratory to develop and certify new prototypes under civil or military aviation regulations. Moreover, the experimental thermo-vacuum chamber can be used for research and development of space technologies and its testing in different simulated space environments. The innovative tailor-made thermo-vacuum chamber presented here was designed to enable test procedures in simulated Martian atmospheric conditions (vacuum of 50 Pa absolute, temperatures up to -125 °C and pure CO2 environment of 1000 Pa absolute). The vacuum tightness of the chamber, the deep cooling of the tested sample under a vacuum environment, the thermal insulations or the heat transfer paths had to be precisely considered. The verification tests of the facility design then proved excellent performance and viability for future technology modifications. This paper reflects the market needs to test airborne and space equipment in different vacuum-cryogenic and thermally controlled extreme conditions.

  • Czech name

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

  • OECD FORD branch

    20304 - Aerospace engineering

Result continuities

  • Project

    <a href="/en/project/LO1202" target="_blank" >LO1202: NETME CENTRE PLUS</a><br>

  • Continuities

    P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Others

  • Publication year

    2018

  • Confidentiality

    S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Data specific for result type

  • Article name in the collection

    ICAS 2018 - PROCEEDINGS

  • ISBN

    978-3-932182-88-4

  • ISSN

  • e-ISSN

  • Number of pages

    9

  • Pages from-to

    1-9

  • Publisher name

    The International Council of the Aeronautical Sciences

  • Place of publication

    ICAS 2018, Belo Horizonte, Brazílie

  • Event location

    Belo Horizonte

  • Event date

    Sep 9, 2018

  • Type of event by nationality

    WRD - Celosvětová akce

  • UT code for WoS article