DocumentCode
2769709
Title
Team Xc: JPL´s collaborative design team for exploring CubeSat, NanoSat, and SmallSat-based mission concepts
Author
Zarifian, Pez ; Imken, Travis ; Matousek, Steve E. ; Moeller, Robert C. ; Bennett, Matthew W. ; Norton, Charles D. ; Rosenberg, Leigh ; Alibay, Farah ; Spangelo, Sara ; Banazadeh, Payam ; Casillas, Raul Polit ; Kawata, Jessie
Author_Institution
Jet Propulsion Lab., Pasadena, CA, USA
fYear
2015
fDate
7-14 March 2015
Firstpage
1
Lastpage
10
Abstract
Recently there has been an increasing demand for a rapid mission concept generation capability for CubeSats, NanoSats, and SmallSats at JPL and in the broader community in the Concept Maturity Level (CML) 2-5 range. To help address these needs, JPL´s Innovation Foundry has extended its long-standing advanced concepts concurrent engineering team, Team X, with a new, agile, and collaborative design capability called Team Xc. This concurrent team-based approach provides rapid turnaround for small spacecraft mission and system early concept studies. The process is adaptable to a wide variety of CubeSat, NanoSat, and SmallSat customers and mission applications. Team Xc design and analysis services include feasibility assessments, trade space exploration studies, and point design studies, commensurate with the level of maturity of the mission concept. The team is assembled with experts experienced in designing, building, launching, and operating CubeSats; leaders in mission architecture, spacecraft design, and concurrent engineering methods; and subject matter experts tailored to the specific needs of each study and customer. The Team Xc capability has been applied to several studies and extended to cover a large breadth of missions spanning applications including Earth science, planetary science, astrophysics, and technology demonstration. Team Xc draws from Team X, JPL, and external subject matter experts to produce quick-turnaround reports targeted to each customer´s needs.
Keywords
artificial satellites; CML 2-5 range; CubeSat; Earth science; JPL collaborative design team; NanoSat; SmallSat-based mission concepts; Team Xc analysis services; Team Xc design; astrophysics; collaborative design capability; concept maturity level; concurrent engineering methods; concurrent team-based approach; mission architecture; planetary science; small spacecraft mission; spacecraft design; technology demonstration; Mars; Propulsion; Solid modeling; Space exploration; Space vehicles; Three-dimensional displays;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2015 IEEE
Conference_Location
Big Sky, MT
Print_ISBN
978-1-4799-5379-0
Type
conf
DOI
10.1109/AERO.2015.7119221
Filename
7119221
Link To Document