X353-5B PROPULSION SYSTEM FLIGHTWORTHINESS RATING TEST

Abstract

This specification defines the flightworthiness rating test requirements for the X353-5B convertible, ducted lift fan propulsion system. The X353-5B propulsion system is comprised of a J85-GE-5 turbojet engine, less afterburner, used as a gas generator plus two additional major components: a diverter valve to direct the gas flow; and an X353-5B lift fan.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1962
Accession Number
AD0634945

Entities

Organizations

  • General Electric

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Army Aviation
  • Contracts
  • Engines
  • Frequency
  • Generators
  • Government (Foreign)
  • Government Procurement
  • Governments
  • Lift Fans
  • Measurement
  • Propulsion System Components
  • Propulsion Systems
  • Sea Level
  • Steady State
  • Turbojet Engines
  • Vibration

Readers

  • Aerospace Engineering