Preliminary Airworthiness Evaluation AH-1S Helicopter Equipped with a Garrett Infrared Radiation Suppressor and an AN/ALQ-144 Jammer.

Abstract

The tests were conducted to determine the effects of installation of the IRS and the AN/ALQ-144 infrared jammer. There was no apparent effect on power required to hover and only a small increase in power required to maintain level flight. Because of a power-available degradation, however, there was a loss of 220 pounds payload in an out-of-ground-effect hover at 4000 feet, 35 C. Additionally, at 2000 feet, 25 c, and 9300 pounds gross weight, there was a reduction in maximum level flight airspeed of 3.5 knots true airspeed in the clean wing configuration. No degradation in handling qualities was caused by IRS or infrared jammer installation. However, one deficiency and six shortcomings inherent in the basic AH-1S were noted. The nonadjustable ventilation system is a deficiency because it blows dirt and dust into the pilot's eyes during operations from unprepared surfaces.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1978
Accession Number
ADA067757

Entities

People

  • Charles E. Frankenberger Jr.
  • Edward E. Bailes
  • Gary L. Bender
  • Sherwood C. Spring

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Ground and Sea Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Acquisition
  • Aircraft Equipment
  • Aircrafts
  • Army Aviation
  • Control Systems
  • Data Acquisition
  • Data Analysis
  • Engineering
  • Ground Effect
  • Helicopters
  • Infrared Radiation
  • Instrumentation
  • Level Flight
  • Manufacturing
  • Performance Tests
  • Test And Evaluation
  • United States

Readers

  • Aerospace Engineering
  • Aerospace Test and Evaluation