Accession Number:

AD0613339

Title:

ENGINE AND WHIRL TESTS, XV-9A HOT CYCLE RESEARCH AIRCRAFT

Descriptive Note:

Summary rept.

Corporate Author:

HUGHES TOOL CO CULVER CITY CA AIRCRAFTDIV

Personal Author(s):

Report Date:

1965-02-01

Pagination or Media Count:

214.0

Abstract:

A summary of engine and whirl testing of the rotor and power module portion of the XV-9A is presented. The results of engine testing include operation of two gas generators into a common exhaust duct with transient power conditions. Rotor whirl test results of the hot cycle rotor used on the XV-9A are reported and include functional check-out, performance evaluation and structural evaluation. Results of testing of a jet-reaction yaw control valve are included.

Subject Categories:

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

Distribution Statement:

APPROVED FOR PUBLIC RELEASE