DocumentCode :
2441576
Title :
Providing the Optimum Solution: Managing Design During Concept Development
Author :
Cuplin, Linda
Author_Institution :
Lockheed Martin Space Syst. Co., Denver
fYear :
2007
fDate :
3-10 March 2007
Firstpage :
1
Lastpage :
9
Abstract :
In a business climate of expanding need, limited resources, and program challenges, it is difficult to sustain a program throughout its life cycle. The impact of this environment has been an increase in the number of concept studies, often with multiple competitive phases. While the intent is to produce an effective system, the atmosphere allows inefficiencies and challenges that are often detrimental to program optimization, often times impeding program completion. Developing a program philosophy that addresses the customer´s changing needs while maintaining the design balance necessary to successfully maintain program advocacy and pass key milestones is critical. A concept development plan should include tools that allow the details to change while retaining the needs of the customer and user community. Utilizing tools such as quality function deployment at the system level ensures that near term customer needs are addressed while maintaining focus on customer expectations and user satisfaction. Successfully implementing sound practices, coupled with creative thinking, promotes a winning solution for the customer, user, and the contractor.
Keywords :
customer satisfaction; quality function deployment; space research; concept development plan; customer expectations; life cycle; optimum solution; pass key milestones; program advocacy; program completion; program optimization; quality function deployment; user community; user satisfaction; Atmosphere; Biographies; Companies; Cost function; History; Impedance; Manufacturing industries; Postal services; Quality control; Quality function deployment;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2007 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
1-4244-0524-6
Electronic_ISBN :
1095-323X
Type :
conf
DOI :
10.1109/AERO.2007.353022
Filename :
4161723
Link To Document :
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