Development, Acquisition, and Operating and Support Cost Methods for Aircraft Turbine Engines,
Abstract
The class of engine discussed in this paper is large, man-rated engines that have thrust levels ranging from a few thousand pounds to approximately 50,000 pounds. The development costs can be as much as a half a billion dollars, with unit costs for some in excess of a million dollars.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1978
- Accession Number
- ADA093821
Entities
People
- J. R. Nelson
- John L. Birkler
Organizations
- RAND Corporation