Hawk Summation
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 November 1975
Abstract
THE Hawk is a low cost/low‐cost‐of‐ownership, close air support/ground attack aircraft designed for world‐wide operation. Having a gross take‐off mass of about 16,000 lb and powered by the Rolls‐Royce Turboméca Ltd Adour Mk. 151 turbofan developing some 23,8 kN (5340 lb) sea‐level static thrust.
Citation
(1975), "Hawk Summation", Aircraft Engineering and Aerospace Technology, Vol. 47 No. 11, pp. 18-21. https://doi.org/10.1108/eb035285
Publisher
:MCB UP Ltd
Copyright © 1975, MCB UP Limited