NASA Logo

NTRS

NTRS - NASA Technical Reports Server

The auto‑search feature has been disabled based on user feedback. Enter a search term/phrase and click “Search” to begin.

Back to Results
Cassini-Huygens Aerodynamics with Comparison to FlightAn analysis has been performed on the aerodynamics of the Cassini spacecraft as it passed through the atmosphere of Titan with and without the Huygens probe attached. The free stream density of Titan s atmosphere was measured by two methods. However, these methods resulted in very different values of density, one result being 3-5 times higher than the other. In an attempt to understand the source of this discrepancy and verify the assumptions made by and the original engineering analysis performed by the Jet Propulsion Laboratory (JPL), free molecular and direct simulation Monte Carlo (DSMC) analyses were performed for two atmospheric passes. The drag coefficient was calculated using an area based on a Monte Carlo area determination program. Although the source of the discrepancy has not been determined, it has been confirmed that the original, simplified force-and-moment analysis performed by JPL produced results that were comparable to the high-fidelity DSMC analysis and that the source of the discrepancy lies elsewhere.
Document ID
20060047648
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Liechty, Derek S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2006
Subject Category
Aerodynamics
Meeting Information
Meeting: 25th International Symposium on Rarefied Gas Dynamics
Location: Saint Petersburg
Country: Russia
Start Date: July 21, 2006
End Date: July 28, 2006
Funding Number(s)
WBS: WBS 23-104-08-50
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available