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Ares I Avionics IntroductionThe Ares I is the next generation human-rated launcher for the United States Constellation program. This system is required to provide single fault tolerance within defined crew safety and mission reliability limits. As part of the effort to achieve those safety goals, Ares I includes an avionics subsystem built as a multistring, voting architecture. The avionics design draws upon experience gained from building fly-by-wire systems for Shuttle, X- 38, and Seawolf. Architectural drivers for the avionics design include using proven technologies with existing suppliers of space rated parts for critical functions (to reduce overall development risk), easing the software development effort by using an off-theshelf, DO-178B certifiable, ARINC-653 operating system in the main flight computers, minimizing mutual data and power connections that might lead to a common-mode hardware failure of the redundant avionics strings, and centralizing overall Ares I command & control within the Upper Stage.
Document ID
20100011081
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Marchant, Christopher C.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 24, 2013
Publication Date
November 10, 2009
Subject Category
Spacecraft Instrumentation And Astrionics
Report/Patent Number
M09-0732
M10-0290
M10-0291
Report Number: M09-0732
Report Number: M10-0290
Report Number: M10-0291
Meeting Information
Meeting: NASA/ARMY Software and Systems Forum
Location: Huntsville, AL
Country: United States
Start Date: May 11, 2010
End Date: May 13, 2010
Sponsors: Society of Automotive Engineers, Inc.
Funding Number(s)
CONTRACT_GRANT: NNM05AB50C
Distribution Limits
Public
Copyright
Public Use Permitted.
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