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Entry, Descent, and Landing Operations Analysis for the Genesis Re-Entry CapsuleOn September 8, 2004, the Genesis spacecraft returned to Earth after spending 29 months about the sun-Earth libration point collecting solar wind particles. Four hours prior to Earth arrival, the entry capsule containing the samples was released for entry and subsequent landing at the Utah Test and Training Range. This paper provides an overview of the entry, descent, and landing trajectory analysis that was performed during the Mission Operations Phase leading up to final approach to Earth. The operations effort accurately delivered the entry capsule to the desired landing site. The final landing location was 8.3 km from the target, and was well within the allowable landing area. Preliminary reconstruction analyses indicate that the actual entry trajectory was very close to the pre-entry prediction.
Document ID
20050060761
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)
Lyons, Dan T.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 7, 2013
Publication Date
January 20, 2005
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AAS-05-121
Report Number: AAS-05-121
Meeting Information
Meeting: 15th AAS/AIAA Space Flight Mechanics Conference
Location: Copper Mountain, CO
Country: United States
Start Date: January 23, 2005
End Date: January 27, 2005
Sponsors: American Inst. of Aeronautics and Astronautics, American Astronomical Society
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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