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タイトルThe Best Estimated Trajectory Analysis for Pad Abort One
本文(外部サイト)http://hdl.handle.net/2060/20110010892
著者(英)Beck, Roger; Kutty, Prasad; Noonan, Meghan; Karlgaard, Christopher
著者所属(英)NASA Dryden Flight Research Center
発行日2011-01-04
言語eng
内容記述I. Best Estimated Trajectory (BET) objective: a) Produce reconstructed trajectory of the PA-1 flight to understand vehicle dynamics and aid other post flight analyses. b) Leverage all measurement sources taken of vehicle during flight to produce the most accurate estimate of vehicle trajectory. c) Generate trajectory reconstructions of the Crew Module (CM), Launch Abort System (LAS), and Forward Bay Cover (FBC). II. BET analysis was started immediately following the PA-1 mission and was completed in September, 2010 a) Quick look version of BET released 5/25/2010: initial repackaging of SIGI data. b) Preliminary version of BET released 7/6/2010: first blended solution using available sources of external measurements. c) Final version of BET released 9/1/2010: final blended solution using all available sources of data.
NASA分類Launch Vehicles and Launch Operations
レポートNODFRC-E-DAA-TN2681
権利Copyright, Distribution under U.S. Government purpose rights
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/247544


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