WESSEX H.C. MK. 2 HELICOPTER XR 588 (TWO GNOME ENGINES MK. 11001 AND 11101) PERFORMANCE AND HANDLING TRIALS IN A MOUNTAINOUS AREA

Abstract

Tests are described which were made on a Wessex Mk. 2 helicopter in the French Alps to assess its take-off and landing capability at altitude. Vertical performance results and handling recommendations are given. It was found that the altitude capability of the Wessex Mk. 2 in vertical flight was limited by the directional control available rather than by engine power.

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Document Details

Document Type
Technical Report
Publication Date
Jan 25, 1965
Accession Number
AD0361138

Entities

People

  • C. R. Verry
  • J. D. Gregory

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Altitude
  • Corporations
  • Directional
  • Flight
  • Government (Foreign)
  • Government Procurement
  • Governments
  • Ground Effect
  • Helicopters
  • High Altitude
  • Hovering
  • Maneuvers
  • Measurement
  • National Security
  • Performance Tests
  • Tail Rotors

Readers

  • Aerospace Test and Evaluation
  • Aviation Safety and Air Traffic Management
  • Seismology