COMMERCIAL SUPERSONIC TRANSPORT PROGRAM. PHASE 2-C. PROPULSION SYSTEM PERFORMANCE SPECIFICATION. PRATT AND WHITNEY AIRCRAFT JTF 17A-20B ENGINE INSTALLATION

Abstract

This specification defines the installed performance of the 650- pound-per-second Pratt and Whitney JTF17A-20B engine in the Boeing Model 733-394 airplane. Performance data are presented for the initial service (1900 F) engine and the basic (2200 F) engine. The estimated inlet drag values used for the determination of airplane performance characteristics are also specified. System performance requirements established herein are design objectives to be applied to the prototype airplanes. Application of these requirements to production airplane design will be established after prototype flight testing.

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Document Details

Document Type
Technical Report
Publication Date
Nov 15, 1965
Accession Number
AD0378635

Entities

Organizations

  • Boeing

Tags

DTIC Thesaurus Topics

  • Aircrafts
  • Airplanes
  • Calorific Value
  • Coefficients
  • Control Systems
  • Department Of State
  • Engines
  • Flight Testing
  • Gas Turbine Nozzles
  • Induction Systems
  • Nozzles
  • Propulsion Systems
  • Sea Level
  • Specifications
  • Standards
  • Supersonic Transport Aircraft
  • United States Government

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Internal Combustion Engine (ICE) Technology.
  • Software Engineering

Technology Areas

  • Hypersonics