Orion Crew Exploration Vehicle Launch Abort System Guidance and Control Analysis Overview

Aborts during the critical ascent flight phase require the design and operation of Orion Crew Exploration Vehicle (CEV) systems to escape from the Crew Launch Vehicle (CLV) and return the crew safely to the Earth. To accomplish this requirement of continuous abort coverage, CEV ascent abort modes ar...

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Bibliographische Detailangaben

Hauptverfasser:	Davidson, John B., Kim, Sungwan, Raney, David L., Aubuchon, Vanessa V., Sparks, Dean W., Busan, Ronald C., Proud, Ryan W., Merritt, Deborah S.
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Launch Vehicles And Launch Operations
Online-Zugang:	Volltext bestellen
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