Further development of the MK 1000
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 October 1973
Abstract
THERE HAS BEEN a continuous improvement in capability of the F28 since its certification in February 1969. This development is depicted in maximum design weight growth and the operational envelope given in fig 11. It shows the advantage of the strength potential, demonstrated by the structural test programme results so that only local modifications were needed.
Citation
(1973), "Further development of the MK 1000", Aircraft Engineering and Aerospace Technology, Vol. 45 No. 10, pp. 14-19. https://doi.org/10.1108/eb035086
Publisher
:MCB UP Ltd
Copyright © 1973, MCB UP Limited