The report describes a feasibility model microwave Instrument Landing System (ILS) developed for the Federal Aviation Agency. Transmitted Frequency: 15.4 kmc, Localizer Clearance: plus or minus 45 degrees, Glide Slope Clearance: plus or minus 15 degrees. System has been successfully demonstrated at NAFEC.
V/STOL Approach System
1966
26 pages
Report
No indication
English
A common design approach to STOL and Y/STOL transport aircraft
Emerald Group Publishing | 1972
|V/STOL Approach System Flight Tests
NTIS | 1966
|Engineering Index Backfile | 1960