SUMMARY OF NAVY STUDY PROGRAM FOR F4H-1 WEAPON SYSTEM. APPENDIX TO VOLUME XII

Abstract

This report presents basic aircraft data and some of the basic performance data (21 November 1958) for the F4H-1 interceptor. A brief description of the F4H-1 is given. The stability derivatives of the F4H-1 are presented in both wind axes and body axes forms for maximum and cruise speed conditions of the F4H-1 at altitudes of 1,000 feet, 30,000 feet and 50,000 feet. The airplane characteristics for both the lateral and longitudinal stick fixed modes are presented. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1958
Accession Number
AD0368417

Entities

Organizations

  • United States Naval Research Laboratory

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aircrafts
  • Airframes
  • Airplanes
  • Altitude
  • Aspect Ratio
  • Coefficients
  • Engines
  • Equations
  • Equations Of Motion
  • High Altitude
  • Jet Engines
  • Low Altitude
  • Mach Number
  • Military Research
  • Steady State
  • Weapon Systems

Readers

  • Aerodynamics/Aeronautics.
  • Missile Defense Systems.
  • Technical Research and Report Writing.