OPERATIONAL TEST AND EVALUATION A/A 37U-15 TOW SYSTEM ON THE F-100 AIRCRAFT.

Abstract

This evaluation was the operational test of the A/A 37U-15 Tow Subsystem with the F-100D aircraft. Missions were conducted to test the tow subsystem for ground and airborne compatibility with the F-100D aircraft. The operation of the tow subsystem during launch and tow and performance capabilities while flying actual dart firing missions were evaluated. It was concluded from the test that the tow subsystem can be satisfactorily used in normal towing operations with the F-100D aircraft. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1967
Accession Number
AD0423429

Entities

People

  • Bobby G. Vinson
  • John B. Cutler
  • Walsie W. Owens

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Test And Evaluation

Readers

  • Aerospace Engineering
  • Marine Hydrodynamics
  • Materials Science and Engineering.