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Computational and Experimental Technique for Selecting Chamber Parameters for Thermal Condition Testing of Onboard Equipment in Unpressurised Spacecraft
Authors: Alekseev V.A., Kudryavtseva N.S., Titova A.S. | Published: 09.04.2018 |
Published in issue: #2(119)/2018 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
Keywords: spacecraft, temperature control systems, thermal vacuum chamber, climate chamber, onboard equipment, unpressurised compartment, Electronic and Electromechanical (EEE) parts |