Accession Number:

AD0631413

Title:

GROUND AND FLIGHT TESTS, XV-9A HOT CYCLE RESEARCH AIRCRAFT

Descriptive Note:

Summary rept., 10 Aug 1964-5 Feb 1965

Corporate Author:

HUGHES TOOL CO CULVER CITY CA AIRCRAFTDIV

Personal Author(s):

Report Date:

1966-03-01

Pagination or Media Count:

183.0

Abstract:

The performance, structural qualities, and feasibility of the Hot Cycle rotor and propulsion system were successfully verified for all normal helicopter flight modes. Ground tests consisted of preflight and tie-down tests, which provided a functional checkout of the aircraft systems and test instrumentation and a final checkout of the completed aircraft prior to start of flight tests. The 15 hours of flight testing included evaluation of aircraft and rotor system performance, flight loads, cooling, and flying qualities in various flight modes.

Subject Categories:

  • Helicopters
  • VSTOL
  • Research and Experimental Aircraft
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE