Powerplant: A brief description of the Spey 512 and RB.162 booster

Abstract

THE Trident 2E is fitted with a further development of the Rolls‐Royce Spey RB.163–25 turbofan engine, designated the Spey 25 Mk. 512–5W. This engine develops a nominal 12,000 lb. take‐off thrust for a dry weight of 2,590 lb.

Citation

(1969), "Powerplant: A brief description of the Spey 512 and RB.162 booster", Aircraft Engineering and Aerospace Technology, Vol. 41 No. 4, pp. 24-28. https://doi.org/10.1108/eb034493