ENGINEERING FLIGHT TEST OF THE AH-1G (HUEYCOBRA) HELICOPTER EQUIPPED WITH THE XM-28 CHIN TURRET WITH TWIN XM-129, 40MM GRENADE LAUNCHERS, PHASE B, PART 4

Abstract

Firing tests were conducted to determine the effects on the stability and control characteristics of the AH-1G helicopter caused by firing the twin XM-129, 40mm grenade launchers in the XM-28 chin turret.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1968
Accession Number
AD0836901

Entities

People

  • Gary C. Hall
  • John R. Melton

Organizations

  • Edwards Air Force Base

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Aircrafts
  • Ammunition
  • Army Aviation
  • Engineering
  • Firing Rate
  • Grenade Launchers
  • Grenades
  • Gun Mounts
  • Guns
  • Helicopters
  • High Explosives
  • Instrumentation
  • Test And Evaluation
  • Test Methods
  • Weapons

Readers

  • Aerodynamics.
  • Aerospace Engineering
  • Munitions and Ordnance Engineering