COMMERCIAL SUPERSONIC TRANSPORT ENGINE. VOLUME XI E. DEVELOPMENT COSTS. PHASE II-A DATA SUBMISSION.

Abstract

This volume includes the estimated development costs for the STF219-B and STF219-L turbofan engines. These Phase II-A engine designs have evolved from optimization studies with the aircraft manufacturers. Primarily as a result of the difference in aircraft configuration, Lockheed's selection indicated an engine size larger than that selected by Boeing. These engines have been designated the STF219-L (Lockheed) and STF219-B (Boeing).

Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1964
Accession Number
AD0804063

Entities

Organizations

  • Pratt & Whitney

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Engines
  • Optimization
  • Supersonic Transport Aircraft
  • Transport Ships
  • Turbofan Engines
  • Vehicles

Readers

  • Business Analytics
  • Internal Combustion Engine (ICE) Technology.
  • Naval Engineering and Maritime Security

Technology Areas

  • Hypersonics