Title :
YCH-60 airborne mine countermeasures proof of concept demonstration
Author :
McConvey, LT Wade ; Michaels, LT Clay
Author_Institution :
Naval Rotary Wing Aircraft Test Squadron, Patuxent River, MD, USA
Abstract :
The investigation of transitioning the Airborne Mine Countermeasures (AMCM) mission to the H-60 helicopter platform required the demonstration of the capability to tow water-borne weapon systems from a YCH-60 prototype aircraft. Naval Rotary Wing Aircraft Test Squadron (NRWATS) was tasked to conduct a multi-phased test during the concept demonstration. The purpose of the Phase I and II testing was to investigate the YCH-60 aircraft capability to conduct the AMCM tow mission under dynamic conditions. Specifically, the test was designed to evaluate aircraft performance and handling qualities, to evaluate adequacy of structural towing provisions, to evaluate design tow speeds and tensions, and to collect usage spectrum data. Flight tests were conducted during a joint Navy and Sikorsky Aircraft Corporation flight test from 17 November 1999 to 17 January 2000. This paper addresses the results and evaluations of Phases I and II
Keywords :
aircraft control; aircraft testing; attitude control; helicopters; human factors; military aircraft; weapons; H-60 helicopter platform; YCH-60 prototype aircraft; airborne mine countermeasures; attitude control; design tow speeds; dynamic conditions; flexible link; flight test; human factors; proof of concept demonstration; structural towing provision; tow water-borne weapon systems; towed sonar; usage spectrum dat; Aerospace electronics; Aircraft manufacture; Aircraft propulsion; Helicopters; Military aircraft; Prototypes; Rivers; Sonar detection; System testing; Weapons;
Conference_Titel :
Aerospace Conference, 2001, IEEE Proceedings.
Conference_Location :
Big Sky, MT
Print_ISBN :
0-7803-6599-2
DOI :
10.1109/AERO.2001.931224