Hover Performance of a Remotely Piloted Helicopter

Abstract

This paper discusses the hover performance of a remotely piloted helicopter (RPH) and the suitability of the use of this RPH in the academic environment of the Naval Postgraduate School Aeronautical Engineering Department. The methods used are those used in the Helicopter Performance Test Manual of the U.S. Navy Test Pilot School. When testing remotely piloted aircraft for use with the military, there is a necessity to test a product to specifications. These specifications may be similar to those of a full sized aircraft. The test methods used are adequate for the testing of RPH's for specification but the use of this equipment in an academic environment is not safe enough without major modification. The RPH has enough excess lift to carry a small test instrumentation package in forward flight. If the RPH is used only in a laboratory environment for the demonstration of hover performance; the gas engine can be replaced with an electric motor and a plexiglas shield can be used between the students and the RPH to satisfy necessary safety precautions.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1986
Accession Number
ADA176587

Entities

People

  • Randolph P. Cotten

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Air Platforms
  • Autonomy
  • Energy and Power Technologies
  • Human Systems

DTIC Thesaurus Topics

  • Aircrafts
  • Electric Motors
  • Engineering
  • Fixed Wing Aircraft
  • Flight
  • Free Flight
  • Instrumentation
  • Load Cells
  • Measurement
  • Measuring Instruments
  • Performance Tests
  • Power Measurement
  • Remotely Piloted Vehicles
  • Schools
  • Standards
  • Telemetry Equipment
  • Test Equipment

Readers

  • Aerospace Engineering
  • STEM Education
  • Systems Analysis and Design