Hostname: page-component-cd9895bd7-gvvz8 Total loading time: 0 Render date: 2024-12-28T06:59:29.894Z Has data issue: false hasContentIssue false

A Resumé of the F-111 Flight Test Programme

Published online by Cambridge University Press:  04 July 2016

Val E. Prahl*
Affiliation:
General Dynamics, Fort Worth Division

Extract

Among the most interesting aircraft development programmes currently in progress is the Flight Test Programme of the F-111, an aeroplane that is being built for both the USAF (the F-111 A) and the US Navy (F-111B). Although the operational envelope of this aeroplane is only a modest step forward into new regions of flight, the dictates of its multi-mission role over the largest Mach-altitude envelope ever achieved by a tactical aeroplane is a significant advancement in the “state of the art”.

To accomplish these mission objectives, which include short take-off and landing distances, sustained supersonic operation at low altitudes, and a Mach 2.5 capability at high altitudes, the F-111 is configured and equipped with a number of unique design features and advanced systems. This discussion is intended to present a brief description of the more interesting features and a progress summary of the F-111 flight test programme.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1968 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)