DocumentCode
3511752
Title
Applying DoDAF to NASA Orion Mission Communication and Navigation Architecture
Author
Biswas, A. ; Hayden, J. ; Phillips, M.S. ; Bhasin, K.B. ; Putt, C. ; Sartwell, T.
Author_Institution
NASA Jet Propulsion Lab., Pasadena, CA
fYear
2008
fDate
1-8 March 2008
Firstpage
1
Lastpage
9
Abstract
NASA´s pursuit of the Vision for Space Exploration (VSE) has motivated the development of an evolvable communication, navigation and timing architecture for crewed missions, initially to the International Space Station (ISS), followed by destinations to the Moon and eventually Mars. A cost-effective, phased development, leveraging to the maximum extent possible existing and upgradable infrastructure, both within and outside NASA, is being emphasized. The transportation of cargo and crew to the ISS using the Crew Exploration Vehicle (CEV), Orion, is currently under development. During this initial mission phase Internet Protocol (IP) based communications, servicing an interoperable System- of-Systems will be developed. The Department of Defense Architecture Framework (DoDAF) processes and prescribed products therein are being used to implement an end-to-end architecture developed using NASA System Engineering practices. In this paper we will provide an overview of the architecting process with a few examples of the NASA applied DoDAF products.
Keywords
Mars; Moon; navigation; space communication links; space vehicles; Department of Defense architecture framework; DoDAF; International Space Station; Internet protocol; Mars; Moon; NASA Orion mission communication; cargo transportation; crew exploration vehicle; interoperable system-of-systems; navigation architecture; timing architecture; vision for space exploration; International Space Station; Internet; Mars; Moon; NASA; Navigation; Road transportation; Space exploration; Timing; Vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2008 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4244-1487-1
Electronic_ISBN
1095-323X
Type
conf
DOI
10.1109/AERO.2008.4526327
Filename
4526327
Link To Document