The purpose of the F-102A Modification and Instrumentation Program was to make the F-102A aircraft compatible with the Landing Control, Central, AN/GSN-5A. Included in the program were: the modification of the automatic flight control system; the design, fabrication and installation of the instrumentation package, corner reflector, automatic throttle and automatic decrab systems. A flight test program was conducted and delivery acceptance of the modified aircraft was made by FAA/BRD upon the completion of ten consecutive 'hands' off automatically-controlled approaches and landings. (Author)
F-102a Modification and Instrumentation Program
1963
2 pages
Report
No indication
English
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