INSTALLED SYSTEMS FUNCTIONAL TEST SUMMARY

Abstract

The the XV-5A aircraft S/N 24506 was ground tested in all areas pertaining to hover, forward fan supported flight, and low speed conventional flight and is acceptable to proceed into active flight testing.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1964
Accession Number
AD0645998

Entities

Organizations

  • General Electric

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aircraft Equipment
  • Aircrafts
  • Army Aviation
  • Cockpits
  • Control Panels
  • Control Sticks
  • Control Surfaces
  • Frequency
  • Fuselages
  • Government Procurement
  • Governments
  • Horizontal Stabilizers
  • Landing Gear
  • Resonant Frequency
  • Trim Tabs
  • Vibration

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Software Engineering