Separation Characteristics of the SUU-51/B from the F-4C Aircraft

Abstract

A wind tunnel test was conducted using 0.05-scale models to study the separation characteristics of the SUU-51/B from the F-4C aircraft. The separation trajectories were initiated from the left-wing inboard pylon station utilizing the Triple Ejection Rack and from the centerline pylon utilizing the Multiple Ejection Rack. The flight conditions simulated were Mach numbers from 0.66 to 0.90 at an altitude of 5000 ft. Parent aircraft dive angles of 0, 30, and 45 deg were simulated.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1971
Accession Number
AD0885843

Entities

People

  • Janis Kukainis

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Acquisition
  • Air Force
  • Aircraft Models
  • Aircrafts
  • Control Systems
  • Data Acquisition
  • Dynamic Pressure
  • Ejection
  • Ejectors
  • Folding Fins (Rockets)
  • Mach Number
  • Models
  • Scale Models
  • Test And Evaluation
  • Test Facilities
  • Trajectories
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.