A Quality Engineering Approach to the Determination of the Space Launch Capability of the Peacekeeper ICBM Utilizing Probabilistic Methods

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AIAA-2002-10-6.pdf (281.41 KB)
Author(s)
Kumpel, Amy E.
Barros, Peter. A., Jr.
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Daniel Guggenheim School of Aerospace Engineering
The Daniel Guggenheim School of Aeronautics was established in 1931, with a name change in 1962 to the School of Aerospace Engineering
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http://hdl.handle.net/1853/6295
Abstract
This paper outlines the use of a comprehensive and robust methodology for the conceptual design of an expendable launch vehicle employing the existing Peacekeeper ICBM. This methodology includes an Integrated Product and Process Development (IPPD) approach, coupled with response surface techniques and probabilistic assessments. IPPD aids the decision-maker in accurately projecting performance and economic metric values. It also provides a probabilistic framework to address the inherent uncertainty in vehicle requirements in an analytical manner by representing payload, mission, and design requirements as distributions instead of point values. In short, the methodology utilized in this study is a combination of traditional missile and rocket design and quality engineering techniques. The main goal of this method is to design for the most affordable system possible while ensuring technical feasibility and economic viability. This paper shows how these methods were applied to a proof of concept investigation of the space launch vehicle (SLV) capability of the Peacekeeper ICBM.
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2002-11
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288167 bytes
1905 bytes
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