Accession Number:

ADA023466

Title:

Development and Flight Test of an Advanced Hydrofluidic Stabilization System

Descriptive Note:

Final rept. 23 Nov 1971-10 Jun 1975

Corporate Author:

HONEYWELL INC MINNEAPOLIS MN GOVERNMENT AND AERONAUTICAL PRODUCTS DIV

Report Date:

1976-02-01

Pagination or Media Count:

231.0

Abstract:

The objective of this program is to demonstrate the performance of an advanced hydrofluidic stabilization system that is designed to provide pilot relief modes within a highly reliable, low-cost system. The system was designed, built, and tested to obtain the desired performance, and then subjected to flightworthiness testing to ensure structural integrity. The system was then installed, flight tested, and evaluated in a UH-1M helicopter. The flight test results are discussed.

Subject Categories:

  • Helicopters
  • Fluidics and Fluerics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE