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Solid rocket motor cost modelA systematic and standardized procedure for estimating life cycle costs of solid rocket motor booster configurations. The model consists of clearly defined cost categories and appropriate cost equations in which cost is related to program and hardware parameters. Cost estimating relationships are generally based on analogous experience. In this model the experience drawn on is from estimates prepared by the study contractors. Contractors' estimates are derived by means of engineering estimates for some predetermined level of detail of the SRM hardware and program functions of the system life cycle. This method is frequently referred to as bottom-up. A parametric cost analysis is a useful technique when rapid estimates are required. This is particularly true during the planning stages of a system when hardware designs and program definition are conceptual and constantly changing as the selection process, which includes cost comparisons or trade-offs, is performed. The use of cost estimating relationships also facilitates the performance of cost sensitivity studies in which relative and comparable cost comparisons are significant.
Document ID
19730004130
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Harney, A. G.
(Aerospace Corp. El Segundo, CA, United States)
Raphael, L.
(Aerospace Corp. El Segundo, CA, United States)
Warren, S.
(Aerospace Corp. El Segundo, CA, United States)
Yakura, J. K.
(Aerospace Corp. El Segundo, CA, United States)
Date Acquired
September 2, 2013
Publication Date
August 31, 1972
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-129255
ATR-73(7313-01)-4
Report Number: NASA-CR-129255
Report Number: ATR-73(7313-01)-4
Accession Number
73N12857
Funding Number(s)
CONTRACT_GRANT: NASW-2301
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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