DocumentCode :
2913343
Title :
Space missions trade space generation and assessment using the JPL Rapid Mission Architecture (RMA) team approach
Author :
Moeller, Robert C. ; Borden, Chester ; Spilker, Thomas ; Smythe, William ; Lock, Robert
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
fYear :
2011
fDate :
5-12 March 2011
Firstpage :
1
Lastpage :
11
Abstract :
The JPL Rapid Mission Architecture (RMA) capability is a novel collaborative team-based approach to generate new mission architectures, explore broad trade space options, and conduct architecture-level analyses. RMA studies address feasibility and identify best candidates to proceed to further detailed design studies. Development of RMA first began at JPL in 2007 and has evolved to address the need for rapid, effective early mission architectural development and trade space exploration as a precursor to traditional point design evaluations. The RMA approach integrates a small team of architecture-level experts (typically 6-10 people) to generate and explore a wide-ranging trade space of mission architectures driven by the mission science (or technology) objectives. Group brainstorming and trade space analyses are conducted at a higher level of assessment across multiple mission architectures and systems to enable rapid assessment of a set of diverse, innovative concepts. This paper describes the overall JPL RMA team, process, and high-level approach. Some illustrative results from previous JPL RMA studies are discussed.
Keywords :
architecture; space research; JPL rapid mission architecture; architecture-level analyses; mission science; multiple mission architectures; space missions; trade space exploration; traditional point design evaluations; Aerospace electronics; Collaboration; Object recognition; Real time systems; Space missions;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2011 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
978-1-4244-7350-2
Type :
conf
DOI :
10.1109/AERO.2011.5747652
Filename :
5747652
Link To Document :
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