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Ares V: Overview and StatusNASA has begun preliminary concept work on the vehicle. Over 1,700 alternatives have been investigated since ESAS. Focused on design of EDS, payload shroud, core stage, and RS-68 core stage engines. Recent point of departure update was made following the Lunar Capability Concept Review. Adds additional performance margin using an additional RS-68. Adds half segment on the first stage boosters . Shroud size is dictated by eventual size of Altair lunar lander. Also investigating alternate uses for Ares V not related to human space exploration . Astronomy applications (e.g., large aperture telescopes), . Deep space missions, DoD applications, Other applications.
Document ID
20090043023
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Creech, Steve
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Sumrall, Phil
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Cockrell, Charles E.
(NASA Langley Research Center Hampton, VA, United States)
Burris, Mike
(Science Applications International Corp. Huntsville, AL, United States)
Date Acquired
August 24, 2013
Publication Date
October 12, 2009
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
M09-0797
Report Number: M09-0797
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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