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Entry, Descent, and Landing Operations Analysis for the Stardust Entry CapsuleOn the morning of January 15, 2006, the Stardust capsule successfully landed at the Utah Test and Training range in northwest Utah returning cometary samples from the comet Wild-2. An overview of the entry, descent, and landing (EDL) trajectory analysis that was performed for targeting during the mission operations phase upon final approach to Earth is described. The final orbit determination solution produced an inertial entry flight-path angle of -8.21 deg (the desired nominal value) with a 3-sigma uncertainty of +/-0.0017 deg (2% of the requirement). The navigation and EDL operations effort accurately delivered the entry capsule to the desired landing site. The final landing location was 8.1 km from the target, which was well within the allowable landing area. Overall, the Earth approach operation procedures worked well and there were no issues (logistically or performance based) that arose. As a result, the process of targeting a capsule from an interplanetary trajectory and accurately landing it on Earth was successfully demonstrated.
Document ID
20090004445
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)
Tooley, Jeff
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Kangas, Julie
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2008
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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