DocumentCode :
2274725
Title :
Acquisition strategy and source selection for co-designing a new-development spacecraft
Author :
Taylor, Randall L.
Author_Institution :
Jet Propulsion Lab., Pasadena, CA
fYear :
0
fDate :
0-0 0
Abstract :
NASA´s Prometheus project was authorized to develop a revolutionary solar system exploration capability - a nuclear electric propulsion spacecraft $that would, during its initial flight, orbit three icy moons of Jupiter. An innovative acquisition strategy - including competitive industry studies, parallel government studies, customized rules of engagement, research, and benchmarking - was employed for project formulation. This strategy produced a new paradigm for space system development: co-design. The co-design paradigm was infused into a unique request for proposal process and a streamlined source evaluation board process, resulting in a timely and effective contractor selection. Following contractor selection, the mechanics of co-design were baselined, then modified through experience. The project co-design team successfully completed the project conceptual design and life cycle cost estimate on schedule, meeting or exceeding all requirements. This paper describes the study contract and down-select phases, provides a definition and description of co-design, and recommends future application of the paradigm for major systems developments
Keywords :
aerospace propulsion; design engineering; space vehicles; strategic planning; Jupiter; NASA; Prometheus Project; Request for Proposal process; Source Evaluation Board process; contractor selection; data acquisition strategy; icy moons; life cycle cost estimate; nuclear electric propulsion spacecraft; project formulation; solar system exploration; space system development; Costs; Government; Job shop scheduling; Jupiter; Life estimation; Moon; Proposals; Propulsion; Solar system; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2006 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
0-7803-9545-X
Type :
conf
DOI :
10.1109/AERO.2006.1656164
Filename :
1656164
Link To Document :
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