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.
Powerplant
A brief description of the Spey 512 and RB.162 booster
Aircraft Engineering and Aerospace Technology ; 41 , 4 ; 24-28
1969-04-01
5 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Emerald Group Publishing | 1971
Emerald Group Publishing | 1974
Emerald Group Publishing | 1970
Engineering Index Backfile | 1963