Natural Icing Tests. UH-1H Helicopter.

Abstract

A limited evaluation of the capability of a modified UH-1H helicopter to fly in a natural icing environment was conducted at Fort Lewis, Washington, from 5 February through 23 February 1974. Testing was performed by the United States Army Aviation Systems Test Activity and consisted of 1.7 hours in icing conditions. During this test, four enhancing features, one deficiency, and one shortcoming were noted. There were four enhancing features associated with special equipment. The deficiency is the inability to maintain autorotational rotor speed within operational limits with main rotor ice accumulation. The striking of the tail rotor by the oscillating iced FM antenna is a shortcoming. Based on these tests, artificial icing characteristics observed in previous UH-1H icing tests are representative of natural icing characteristics. The UH-1H helicopter does not possess the capability to operate safely in an icing environment.

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1974
Accession Number
ADA002077

Entities

People

  • Carl F. Mittag
  • James S. Reid
  • Marvin L. Hanks
  • Warren E. Griffith Ii

Organizations

  • Edwards Air Force Base

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Army Aviation
  • Deficiencies
  • Environment
  • Helicopters
  • Tail Rotors
  • Test And Evaluation
  • United States
  • Vehicle Equipment
  • Vehicles

Readers

  • Aerospace Engineering
  • Polar and Arctic Studies