Heavy Lift Helicopter Engine Development Program Design to Cost, 2nd Period Award Fee Evaluation Report.

Abstract

During development of a 8079 shaft horsepower gas turbine engine, the contractor proformed an extensive design to cost effort under an award fee provision. This report summarizes the government's evaluation of this effort and includes a description of the contractor's design to cost policy and procedures.

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1975
Accession Number
ADA016120

Entities

People

  • Conrad W. Faber

Organizations

  • United States Army Aviation and Missile Command

Tags

DTIC Thesaurus Topics

  • Contractors
  • Energy Generators
  • Energy Systems
  • Engines
  • Gas Turbines
  • Generators
  • Helicopter Engines
  • Helicopters
  • Horsepower
  • Mechanical Equipment
  • Test And Evaluation
  • Turbine Components
  • Turbines
  • Turbomachinery

Readers

  • Aerospace Engineering
  • Government Contracting/Procurement.
  • Software Engineering