Separation Trajectories of Various Munitions when Released from the A-7D Aircraft at Mach Numbers from 0.33 to 0.95
Abstract
Wind tunnel captive trajectory tests were conducted in the Aerodynamic Wind Tunnel (4T) to investigate the separation characteristics of various external stores from the wing, pylons, and racks of the A-7D aircraft. Separation trajectory data were obtained for the MK-84 LGB, MK-84 EOGB, MK-82 LGB, and BLU-1/B bombs, and for the loaded and expended LAU-68 A/A rocket launcher. Trajectories were obtained at Mach numbers from 0.33 to 0.95 at simulated altitudes from 4,000 to 15,000 ft. At selected test conditions, parent-aircraft climb angles of 0 to -70 deg were simulated. In general, the stores separated from the aircraft without contacting the wing, pylon, or rack.
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 01, 1973
- Accession Number
- AD0907813
Entities
People
- David W. Hill Jr.
Organizations
- Arnold Engineering Development Complex