| タイトル | Crew Exploration Vehicle Service Module Ascent Abort Coverage |
| 本文（外部サイト） | http://hdl.handle.net/2060/20070024459 |
| 著者（英） | Falck, Robert D.; Tedesco, Mark B.; Merritt, Deborah S.; Evans, Bryan M. |
| 著者所属（英） | NASA Johnson Space Center |
| 発行日 | 2007-08-20 |
| 言語 | eng |
| 内容記述 | The Crew Exploration Vehicle (CEV) is required to maintain continuous abort capability from lift off through destination arrival. This requirement is driven by the desire to provide the capability to safely return the crew to Earth after failure scenarios during the various phases of the mission. This paper addresses abort trajectory design considerations, concept of operations and guidance algorithm prototypes for the portion of the ascent trajectory following nominal jettison of the Launch Abort System (LAS) until safe orbit insertion. Factors such as abort system performance, crew load limits, natural environments, crew recovery, and vehicle element disposal were investigated to determine how to achieve continuous vehicle abort capability. |
| NASA分類 | Spacecraft Design, Testing and Performance |
| 権利 | No Copyright |
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