Accession Number:

AD0477907

Title:

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

Descriptive Note:

Corporate Author:

ARMY TRANSPORTATION RESEARCH COMMAND FORT EUSTIS VA

Personal Author(s):

Report Date:

1964-02-01

Pagination or Media Count:

59.0

Abstract:

A summary is presented of results of flight testing conducted on the UH-2 helicopter, modified by the installation of a YJ85 turbo-jet engine for auxiliary propulsion, throughout the currently established level flight envelope to 140 knots. This testing was conducted in accordance with the Phase I requirements of the referenced contract and substantiates the safety of flight of the helicopter with the jet engine. Author

Subject Categories:

  • Helicopters

Distribution Statement:

APPROVED FOR PUBLIC RELEASE