Military jet engine acquisition : technology basics and cost-estimating methodology / Obaid Younossi [and others].
- Published
- Santa Monica, CA : RAND, 2002.
- Physical Description
- xxii, 153 pages : illustrations (some color) ; 23 cm
- Additional Creators
- Younossi, Obaid, Arena, Mark V., Moore, Richard M., Lorell, Mark A., 1947-, Mason, Joanna, Graser, John C., Project Air Force (U.S.). Resource Management Program, Rand Corporation, and United States. Air Force
Online Version
- www.rand.org , Online access
- Summary
- As manufacturing processes and materials used in aircraft engine production change and new information on aircraft engine technology becomes available, cost-estimation techniques must be updated. The authors present the results of a RAND research project to develop a new methodology for estimating military jet engine costs. They first discuss the technical parameters that drive the engine development schedule, development costs, and production costs, and then present a quantitative analysis of actual historical data on development schedules and costs. Their principal focus was on adding new observations to the cost-estimating database from earlier RAND studies and updating the parametric relationships for aircraft engine costs and development time. The authors present a series of parametric relationships for forecasting the development cost, development time, and production cost of future military engine programs. Their results indicate that rotor inlet temperature is a significant variable in most of the reported estimating relationships. Full-scale test hours and whether an engine is new or derivative were also found to be significant cost-estimating measures.
- Report Numbers
- RAND/MR-1596-AF
- Subject(s)
- Other Subject(s)
- ISBN
- 0833032828 (pbk.)
- Note
- "Project Air Force."
- Bibliography Note
- Includes bibliographical references (pages 147-153).
- Other Forms
- Also available on the internet via WWW in PDF format.
- Funding Information
- Air Force. F49642-01-C-0003. PA002 6783. PA002 3957. PA002 2957
- Complexity Note
- Supersedes RAND/DRR-2650-AF.
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