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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: AD0255537

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.

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