CATEGORY II LOW TEMPERATURE EVALUATION OF A YUH-ID HELICOPTER IN THE ARCTIC.

Abstract

The model YUH-1D helicopter was tested at temperatures down to -51 F in the Arctic at Eielson AFB, Alaska, during the period of 20 December 1962 through 17 January 1963. This report presents the data that was collected during the test and a discussion and analysis of the low temperature deficiencies that were encountered. The most significant deficiencies that were encountered were excessive engine oil pressure during starts below -20 F and erratic operation of the bleed-air driven fuel boost pump. The helicopter can be expected to operate successfully in an Arctic environment if corrective action is taken as outlined in the recommendations of this report. (Author)

Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1963
Accession Number
AD0422643

Entities

People

  • Billy L. White

Tags

DTIC Thesaurus Topics

  • Aircrafts
  • Biological Phenomena
  • Deficiencies
  • Environment
  • Helicopters
  • Low Temperature
  • Test And Evaluation

Readers

  • Aerospace Engineering
  • Aerospace Test and Evaluation
  • Polar and Arctic Studies