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. (Author)


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