Abstract
Spacecraft components may be damaged due to airflow produced by Environmental Control Systems (ECS). There are uncertainties and errors associated with using Computational Fluid Dynamics (CFD) to predict the flow field around a spacecraft from the ECS System. This paper describes an approach to estimate the uncertainty in using CFD to predict the airflow speeds around an encapsulated spacecraft without using test data.
Original language | American English |
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Title of host publication | Proceedings of the Aerospace Sciences Meeting |
DOIs | |
State | Published - Jan 13 2014 |
Keywords
- Computational fluid
- Computational fluid dynamics
- Environmental control system
- Payload fairing
- Spacecraft
DC Disciplines
- Mechanical Engineering