Accession Number:

ADA016932

Title:

Roll-Axis Hydrofluidic Stability Augmentation System Development

Descriptive Note:

Final rept. 29 Mar 1973-30 Sep 1974

Corporate Author:

HONEYWELL INC MINNEAPOLIS MN GOVERNMENT AND AERONAUTICAL PRODUCTS DIV

Report Date:

1975-09-01

Pagination or Media Count:

137.0

Abstract:

The objective of this program was to develop, design, and flight test a roll-axis Hydrofluidic Stability Augmentation System HYSAS for the OH-58A helicopter. The system, when used with a yaw HYSAS, provides increased vehicle damping which improves the handling characteristics. Flight test evaluations were performed with satisfactory results.

Subject Categories:

  • Helicopters

Distribution Statement:

APPROVED FOR PUBLIC RELEASE