F-101A Tow Subsystem System Tests. F-101A Airplane. Part II
Report Number: WADD TR 61-204 Part 2 Author: Green, M. L. Corporate Author: Northrop Aircraft Date of Publication: 1961-05 Pages: 74 AD Number: AD0255537Contrails does not possess a copy of this report. Click here to offer Contrails a donation of this report
Abstract: Results are presented of the flight test program conducted on the F-101A tow subsystem. Two NF-101A aircraft were modified to the test configuration and were used throughout the test program. One of these was chosen as the basic test article and was instrumented to provide quantitative test data.