Separation Characteristics of the ASP Dispenser Munition from the F-4C Aircraft at Mach Numbers from 0.66 to 1.20.

Abstract

Wind tunnel tests were conducted using 0.05-scale models to study the separation characteristics of the ASP Dispenser munition (both with fins open and fins closed) from the F-4C aircraft. The separation trajectories were initiated from the right-wing inboard pylon station utilizing the Triple Ejection Rack and from the parent-aircraft center-line pylon station utilizing the Multiple Ejection Rack. Data were obtained at Mach numbers from 0.66 to 1.20 at a simulated altitude of 5000 ft. Dive angles varied from -45 to 45 deg for simulated parent-aircraft accelerations from 1 to 4g. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1972
Accession Number
AD0890742

Entities

People

  • J. B. Carman

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Altitude
  • Cooperation
  • Dispensers
  • Ejection
  • Ejectors
  • Mach Number
  • Models
  • Munitions
  • Scale Models
  • Trajectories
  • Triple Ejection Racks
  • Weapons
  • Wind Tunnel Tests
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.