Spacecraft thermal protection systems are at risk of being damaged due to airflow produced from Environmental Control Systems (ECS).
Dissertation Defense: Computational Fluid Dynamics Uncertainty Analysis for Payload Fairing Spacecraft Environmental Control Systems
2014
122 pages
Report
Keine Angabe
Englisch
Physics , Fluid Mechanics , Jet & Gas Turbine Engines , Computational fluid dynamics , K-epsilon turbulence model , Turbulent flow , Uncertain systems , Environmental control , Aerodynamic heat transfer , Turbulent heat transfer , Thermodynamics , Temperature control , Thermal protection , Heat shielding
British Library Conference Proceedings | 2014
|Payload fairing separation dynamics
AIAA | 1999
|