DocumentCode
2688283
Title
MIDEX advanced modular and distributed spacecraft avionics architecture
Author
Ruffa, John A. ; Castell, Karen ; Flatley, Thomas ; Lin, Michael
Author_Institution
NASA Goddard Space Flight Center, Greenbelt, MD, USA
Volume
5
fYear
1998
fDate
21-28 Mar 1998
Firstpage
531
Abstract
MIDEX (Medium Class Explorer) is the newest line in NASA´s Explorer spacecraft development program. As part of the MIDEX charter, the MIDEX spacecraft development team has developed a new modular, distributed, and scaleable spacecraft architecture that pioneers new spaceflight technologies and implementation approaches, all designed to reduce overall spacecraft cost while increasing overall functional capability. This resultant “plug and play” system dramatically decreases the complexity and duration of spacecraft integration and test, providing a basic framework that supports spacecraft modularity and scalability for missions of varying size and complexity. Together, these subsystems form a modular, flexible avionics suite that can be modified and expanded to support low-end and very high-end mission requirements with a minimum of redesign, as well as allowing a smooth, continuous infusion of new technologies as they are developed without redesigning the system. This overall approach has the net benefit of allowing a greater portion of the overall mission budget to be allocated to mission science instead of a spacecraft bus. The MIDEX scaleable architecture is currently being manufactured and tested for use on the Microwave Anisotropy Probe (MAP), an in-house program at GSFC
Keywords
avionics; modules; redundancy; space vehicle electronics; space vehicles; Explorer spacecraft development program; MIDEX; Medium Class Explorer; Microwave Anisotropy Probe; NASA; flexible avionics suite; functional capability; overall mission budget; overall spacecraft cost; scalability; scaleable spacecraft architecture; spacecraft avionics architecture; spacecraft modularity; spaceflight technologies; Aerospace electronics; Aircraft manufacture; Anisotropic magnetoresistance; Cost function; Manufacturing; Probes; Scalability; Space technology; Space vehicles; System testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 1998 IEEE
Conference_Location
Snowmass at Aspen, CO
ISSN
1095-323X
Print_ISBN
0-7803-4311-5
Type
conf
DOI
10.1109/AERO.1998.685863
Filename
685863
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