Accession Number:

AD0255537

Title:

F-101A TOW SUBSYSTEM SYSTEM TESTS. F-101A AIRPLANE. PART II

Descriptive Note:

Corporate Author:

NORTHROP AIRCRAFT INC HAWTHORNE CA

Personal Author(s):

Report Date:

1961-04-01

Pagination or Media Count:

1.0

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. Author

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE