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
Link To Document :
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