AS is to be expected, the various systems on the Trident 2E closely follow those evolved for the Tridents 1 and 1E, except for the changes in the fuel system necessitated by the introduction of the fin fuel tank, and the embodiment of a turbine-compressor type of cold air unit in the air conditioning system.
Trident 2E Aircraft Systems
Details of fuel system, electrical power installation, hydraulic system, air conditioning and pressurisation and flying controls
Aircraft Engineering and Aerospace Technology ; 41 , 4 ; 14-24
1969-04-01
11 pages
Article (Journal)
Electronic Resource
English
Emerald Group Publishing | 1971
Operational experience with trident aircraft
Engineering Index Backfile | 1964
|Operational Experience with the Trident Aircraft
SAE Technical Papers | 1964
|AIRCRAFT PROFILE - HAWKER SIDDELEY TRIDENT - Bruce Hales-Dutton details development of the Trident.
Online Contents | 2005
|Engineering Index Backfile | 1964
|