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

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)

Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1961
Accession Number
AD0255537

Entities

People

  • M.l. Green

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airplanes
  • Fixed Wing Aircraft

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Oceanography.