Part Two—Spey By‐Pass Turbojet Engine: Description of the Design Background and Technical Features of the Rolls‐Royce RB.I63 Power Plant
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 January 1962
Abstract
INITIALLY developed to power the new generation of British short and medium range jet airliners, the Rolls‐Royce Spey is a 10,000 lb. thrust by‐pass engine designed for operational economy—low fuel consumption, low maintenance costs and a long overhaul life.
Citation
(1962), "Part Two—Spey By‐Pass Turbojet Engine: Description of the Design Background and Technical Features of the Rolls‐Royce RB.I63 Power Plant", Aircraft Engineering and Aerospace Technology, Vol. 34 No. 1, pp. 7-11. https://doi.org/10.1108/eb033506
Publisher
:MCB UP Ltd
Copyright © 1962, MCB UP Limited