Design and operation of simple thermal vacuum chamber for testing of small spacecraft components

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F19%3A00339507" target="_blank" >RIV/68407700:21220/19:00339507 - isvavai.cz</a>
Result on the web
<a href="https://doi.org/10.1109/NTAD.2019.8875545" target="_blank" >https://doi.org/10.1109/NTAD.2019.8875545</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1109/NTAD.2019.8875545" target="_blank" >10.1109/NTAD.2019.8875545</a>

Result language
angličtina
Original language name
Design and operation of simple thermal vacuum chamber for testing of small spacecraft components
Original language description
A small low-cost thermal vacuum chamber was designed, built and operated. The thermal cycling was done using inner shroud, designed to be used either as a pure cold-wall for radiative cooling or as a thermal contact plate. Computer controlled liquid nitrogen partial flooding system was adopted for cooling and hot air flow was used for heating of the shroud. The thermal vacuum chamber was used for validation of stability of properties of the primer BR 127 outside previously certified temperature range. The tape test (peel-off) of adhesion according to ASTM D3359 09 was done on the primer before and after the thermal-vacuum cycling. The tested primer stood the test without discernible changes of the adhesion properties.
Czech name
—
Czech description
—

Project
<a href="/en/project/FV10400" target="_blank" >FV10400: Development of processes applicable to development and production of components for the space industry</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2019
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Similar results(10)