Accession Number:

ADA093821

Title:

Development, Acquisition, and Operating and Support Cost Methods for Aircraft Turbine Engines,

Descriptive Note:

Corporate Author:

RAND CORP SANTA MONICA CA

Personal Author(s):

Report Date:

1978-09-01

Pagination or Media Count:

63.0

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.

Subject Categories:

  • Civilian Aircraft
  • Administration and Management
  • Economics and Cost Analysis
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE