DocumentCode
2794602
Title
Development of an integrated concurrent design tool for the design of human spaceflight missions
Author
Kwong, Jeffrey ; Mosher, Todd J.
Author_Institution
Mech. & Aerosp. Eng., Utah State Univ., Logan, UT
fYear
2005
fDate
5-12 March 2005
Firstpage
4268
Lastpage
4275
Abstract
Currently, there are few viable integrated concurrent design (ICD) tools that are available for human spaceflight design. To address this shortcoming, recent work has taken place at Utah State University in the development of a human spaceflight design tool to be used in an ICD environment. This tool will allow a group of engineers to rapidly design a short or long duration human mission to the Moon or Mars. All aspects of a mission architecture can be designed using this tool, ranging from transfer vehicles to surface habitats. The functionality of this tool and potential applications that this tool may have are discussed in this paper
Keywords
Mars; Moon; aerospace instrumentation; space vehicles; Mars; Moon; human spaceflight missions; integrated concurrent design tool; surface habitats; transfer vehicles; Aerospace engineering; Automotive engineering; Design engineering; Design methodology; Humans; Mars; Moon; Orbital robotics; Space exploration; Space vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2005 IEEE
Conference_Location
Big Sky, MT
Print_ISBN
0-7803-8870-4
Type
conf
DOI
10.1109/AERO.2005.1559731
Filename
1559731
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