The braking system for a short takeoff aircraft is discussed and the deficiencies are described. The installation of a Boeing 727 aircraft brake system was made to correct the deficiencies. Tests of the modified system were conducted using an analog computer/hardware simulator. Actual performance tests were conducted and the characteristics of the system were satisfactory. (Author)
Brake Control System Modification, Augmentor Wing Jet STOL Research Airplane (Awjsra)
1974
78 pages
Report
Keine Angabe
Englisch