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.

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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

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Acquisition
  • Aircrafts
  • California
  • Contracts
  • Corporations
  • Plastic Explosives
  • Turbines

Readers

  • Aerospace Engineering
  • Logistics and Supply Chain Management.
  • Public Financial Management and Budgeting