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Reconstruction of the Genesis EntryAn overview of the reconstruction analyses performed for the Genesis capsule entry is described. The results indicate that the actual entry prior to the drogue deployment failure was very close to the pre-entry predictions. The capsule landed 8.3 km south of the desired target at Utah Test and Training Range. Analysis on infrared video footage (obtained from the tracking stations) during the descent estimated the onset of the capsule tumble at Mach 0.9. Frequency analysis on the infrared video data indicates that the aerodynamics generated for the Genesis capsule reasonably predicted the drag and static stability. Observations of the heatshield support the pre-entry simulation estimates of a small hypersonic angles-of-attack, since there is very little, if any, charring of the shoulder region or the aftbody. Through this investigation, an overall assertion can be made that all the data gathered from the Genesis entry is consistent with flight performance that was close to the nominal preentry prediction. Consequently, the design principles and methodologies utilized for the flight dynamics, aerodynamics, and aerothermodynamics analyses have been corroborated.
Document ID
20080019649
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Desai, Prasun N.
(NASA Langley Research Center Hampton, VA, United States)
Qualls, Garry D.
(NASA Langley Research Center Hampton, VA, United States)
Schoenenberger, Mark
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2007
Subject Category
Space Sciences (General)
Funding Number(s)
WBS: WBS 439654.02.07.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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