Category II Desert Test of the HH-53C Helicopter. Appendix 3. Volume 3.

Abstract

This run presents data for inflight operation at very high ambient temperature (49C/120F) combined with high gross weight (41,000 lb) and high power operation. Engine topping power checks were accomplished. The usual engine oil and engine nose gearbox oil overheat occurred during hover operations.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1973
Accession Number
AD0911334

Entities

People

  • John L. Barbagallo

Organizations

  • Air Force Test Center

Tags

Communities of Interest

  • Air Platforms
  • C4I
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Compressors
  • Desert Tests
  • Engines
  • Flight
  • Government Procurement
  • Governments
  • Ground Effect
  • High Temperature
  • Intellectual Property
  • Law
  • Nose Wheels
  • Plastic Explosives
  • Surface Temperature
  • Test And Evaluation
  • Three Dimensional

Readers

  • Aerospace Engineering
  • Regression Analysis.