F-4 Rain Tire Performance Flight Test

Abstract

This report presents the results of the F-4 Rain Tire flight test program. A total of 155 test landings were made by an unslatted F-4E on both a dry and wet concrete runway. These tests were done primarily to (1) compare the performance of the Hytrol Mark III antiskid system to the production F-4 antiskid system, the Hytrol Mark II, (2) evaluate the wet runway stopping performance of four new main landing gear tire tread designs, (3) evaluate the directional control performance of three new nosewheel tire tread designs compared with that of the Standard nosewheel tire, and (4) evaluate a pilot-selectable, two-mode authority steering system. Secondary objectives were to determine the effects of tire tread wear, various touchdown sink rates, and no flap/half flap landing configurations on the wet runway stopping performance of the F-4.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1974
Accession Number
AD0922598

Entities

People

  • Larry K. Mccallon

Organizations

  • Air Force Test Center

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Human Systems
  • Sensors
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Control Panels
  • Depth Indicators
  • Drag
  • Energy
  • Flight Speeds
  • Friction
  • Ground Speed
  • Indicators
  • Inertial Navigation
  • Inertial Navigation Systems
  • Landing Gear
  • Measurement
  • Nose Wheels
  • Systems Engineering
  • Test And Evaluation

Readers

  • Aerospace Engineering
  • Pavement Materials Engineering.