ENGINEERING FLIGHT TEST OF UH-1B HELICOPTER EQUIPPED WITH XM-16 ARMAMENT SUBSYSTEM AND ENGINEERING FLIGHT TEST OF UH-1B HELICOPTER EQUIPPED WITH XM-21 ARMAMENT SUBSYSTEM

Abstract

Engineering flight tests of the UH-1B helicopter equipped with the XM-16 and XM-21 armament subsystems were conducted. The overall objective was to determine the effect of the installation of the subsystems on the UH-1B. Specific objectives were to determine the existence of any safety-of-flight conditions by evaluation of equantitative stability and control and vibration data and to determine any performance losses.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1966
Accession Number
AD0488791

Entities

People

  • George M. Yamakawa
  • John K. Foster

Organizations

  • Edwards Air Force Base

Tags

Communities of Interest

  • Air Platforms
  • Ground and Sea Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Airframes
  • Altitude
  • Army Aviation
  • Contractors
  • Engineering
  • Flight
  • Flight Speeds
  • Guns
  • Instrumentation
  • Level Flight
  • Machine Guns
  • Measurement
  • Test And Evaluation
  • Turbines
  • Weapons

Fields of Study

  • Physics

Readers

  • Aerial Unmanned Vehicle Swarm Micro Periodontal Dentistry.
  • Aerospace Engineering
  • Manufacturing Engineering.