PRELIMINARY FLIGHT TEST DATA UH-2A WITH HORIZONTAL THRUST AUGMENTATION PROVIDED BY A YJ-85 TURBO-JET ENGINE.

Abstract

The report summarizes the flight testing conducted on UH-2 helicopter BuNo. 147978, modified by the installation of a YJ85 turbo-jet engine for auxiliary propulsion, during the period 22 January 1964 through 3 Apr 1964. A total of 42 flights, involving 28.3 hours of aircraft time were conducted. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1964
Accession Number
AD0621892

Tags

DTIC Thesaurus Topics

  • Aircrafts
  • Engines
  • Flight Testing
  • Helicopters
  • Jet Engines
  • Rotary Wing Aircraft
  • Thrust
  • Thrust Augmentation
  • Vehicles

Readers

  • Aerospace Engineering
  • Technical Research and Report Writing.