Design Experiences and Flight Test Results from NASA's Max Launch Abort System (MLAS): A Flight Mechanics Perspective (AAS 10-084)
33rd, Rocky Mountain Guidance and Control Conference ; 2010 ; Breckenridge, CO
2010-01-01
28 pages
Includes bibliographical references and indexes. Proceedings of the 33rd Annual AAS Rocky Mountain Guidance and Control Conference.
Conference paper
English
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GN&C Design Overview and Flight Test Results from NASA's Max Launch Abort System (MLAS)
British Library Conference Proceedings | 2010
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