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Spacecraft Design Considerations for Piloted Reentry and LandingWith the end of the Space Shuttle era anticipated in this decade and the requirements for the Crew Exploration Vehicle (CEV) now being defined, an opportune window exists for incorporating 'lessons learned' from relevant aircraft and space flight experience into the early stages of designing the next generation of human spacecraft. This includes addressing not only the technological and overall mission challenges, but also taking into account the comprehensive effects that space flight has on the pilot, all of which must be balanced to ensure the safety of the crew. This manuscript presents a unique and timely overview of a multitude of competing, often unrelated, requirements and constraints governing spacecraft design that must be collectively considered in order to ensure the success of future space exploration missions.
Document ID
20080026216
Acquisition Source
Johnson Space Center
Document Type
Preprint (Draft being sent to journal)
Authors
Stroud, Kenneth J.
(NASA Johnson Space Center Houston, TX, United States)
Klaus, David M.
(Colorado Univ. Boulder, CO, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2006
Subject Category
Spacecraft Design, Testing And Performance
Distribution Limits
Public
Copyright
Public Use Permitted.
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